MATH-283 (Calculus III) Curriculum

Session 07 - Midterm Review 1

Handout Worksheet
Fall Semester 2026
Session Objectives & Overview

By the end of this session, you will be able to:

  • Decompose 3D force and displacement vectors into parallel and perpendicular components using scalar and vector projections, apply dot and cross products to compute work, torque, angles, and geometric areas/volumes, and distinguish scalar vs vector physical quantities.
  • Formulate vector, parametric, and symmetric equations of lines in 3D space, calculate perpendicular point-to-line clearance envelopes, and systematically classify spatial line pairs as parallel, intersecting, skew, or coincident using direction vector ratios and two-parameter linear systems.
  • Differentiate and integrate vector-valued space curves rβƒ—(t)\vec{r}(t)r(t), evaluate arc length and construct intrinsic unit-speed parametrizations rβƒ—(s)\vec{r}(s)r(s), calculate curvature ΞΊ(t)\kappa(t)ΞΊ(t) and osculating radii ρ(t)\rho(t)ρ(t), and decompose kinematic acceleration into tangential and normal components (aβƒ—=aTT^+aNN^\vec{a} = a_T \hat{T} + a_N \hat{N}a=aT​T^+aN​N^) to audit structural and biomechanical dynamic limits.

Micro-Lecture

1. Midterm 1 Strategy & The Physicist-Mathematician-Engineer Triad

  • Mathematical Foundation: Unit 1 of Calculus III transitions our mathematical universe from flat 2D calculus to 3D spatial modeling R3\mathbb{R}^3R3. Success on Midterm Exam 1 requires mastery of the three distinct operational tiers:
    1. Spatial Representation: Mapping geometry using position vectors rβƒ—=⟨x,y,z⟩=xi^+yj^+zk^\vec{r} = \langle x, y, z \rangle = x\hat{i} + y\hat{j} + z\hat{k}r=⟨x,y,z⟩=xi^+yj^​+zk^ (see Vectors) and direction vectors vβƒ—=⟨a,b,c⟩\vec{v} = \langle a, b, c \ranglev=⟨a,b,c⟩.
    2. Vector Multiplication Algebra: Distinguishing scalar output operations (the Dot Product u⃗⋅v⃗\vec{u}\cdot\vec{v}u⋅v and Vector Projections) from orthogonal vector output operations (the Cross Product u⃗×v⃗\vec{u}\times\vec{v}u×v and Triple Scalar Product and Spatial Volume).
    3. Space Curve Differential Geometry: Analyzing particle kinematics (v⃗(t),a⃗(t)\vec{v}(t), \vec{a}(t)v(t),a(t)), intrinsic distance through Arc Length of a Space Curve, turning sharpness via Curvature of a Space Curve, and dynamic force partitioning via Tangential and Normal Components of Acceleration.
  • Engineering Context: On exams, engineers do not perform random algebraic substitutions. We classify the physical system, select the governing vector formula, and state the symbolic equation before executing numerical calculations.

2. Formula Hierarchy & Problem Classification

  • Master the formula hierarchy: identify whether a prompt asks for a scalar (speed, arc length, distance, curvature, work, volume) or a vector (position, velocity, acceleration, unit tangent, normal vector, torque, projection).

Skill Block 1

Worked Example A: Vector Projections, Decomposition, and Cross Product

Given vectors uβƒ—=⟨2,βˆ’1,2⟩\vec{u} = \langle 2, -1, 2 \rangleu=⟨2,βˆ’1,2⟩ and vβƒ—=⟨1,2,2⟩\vec{v} = \langle 1, 2, 2 \ranglev=⟨1,2,2⟩ in R3\mathbb{R}^3R3:

  1. Compute the dot product u⃗⋅v⃗\vec{u} \cdot \vec{v}u⋅v and evaluate the angle θ\thetaθ between them.
  2. Find the scalar projection scaluβƒ—vβƒ—\text{scal}_{\vec{u}}\vec{v}scalu​v and vector projection projuβƒ—vβƒ—\text{proj}_{\vec{u}}\vec{v}proju​v.
  3. Compute the orthogonal vector component orthuβƒ—vβƒ—\text{orth}_{\vec{u}}\vec{v}orthu​v and verify that it is perpendicular to uβƒ—\vec{u}u.
  4. Compute the cross product u⃗×v⃗\vec{u} \times \vec{v}u×v and find the exact geometric area of the parallelogram spanned by u⃗\vec{u}u and v⃗\vec{v}v.
Worked Solution:
  1. Compute Vector Magnitudes and Dot Product: State the Vector Magnitude Formula:

    βˆ₯uβƒ—βˆ₯=u12+u22+u32=22+(βˆ’1)2+22=4+1+4=9=3\|\vec{u}\| = \sqrt{u_1^2 + u_2^2 + u_3^2} = \sqrt{2^2 + (-1)^2 + 2^2} = \sqrt{4 + 1 + 4} = \sqrt{9} = 3βˆ₯uβˆ₯=u12​+u22​+u32​​=22+(βˆ’1)2+22​=4+1+4​=9​=3
    βˆ₯vβƒ—βˆ₯=v12+v22+v32=12+22+22=1+4+4=9=3\|\vec{v}\| = \sqrt{v_1^2 + v_2^2 + v_3^2} = \sqrt{1^2 + 2^2 + 2^2} = \sqrt{1 + 4 + 4} = \sqrt{9} = 3βˆ₯vβˆ₯=v12​+v22​+v32​​=12+22+22​=1+4+4​=9​=3

    State the Dot Product Formula:

    uβƒ—β‹…vβƒ—=u1v1+u2v2+u3v3=(2)(1)+(βˆ’1)(2)+(2)(2)=2βˆ’2+4=4\vec{u} \cdot \vec{v} = u_1 v_1 + u_2 v_2 + u_3 v_3 = (2)(1) + (-1)(2) + (2)(2) = 2 - 2 + 4 = 4uβ‹…v=u1​v1​+u2​v2​+u3​v3​=(2)(1)+(βˆ’1)(2)+(2)(2)=2βˆ’2+4=4
    (Defined in Dot Product.)

    Evaluate angle ΞΈ\thetaΞΈ:

    cos⁑θ=uβƒ—β‹…vβƒ—βˆ₯uβƒ—βˆ₯βˆ₯vβƒ—βˆ₯=4(3)(3)=49β€…β€ŠβŸΉβ€…β€ŠΞΈ=arccos⁑(49)β‰ˆ63.61∘\cos\theta = \frac{\vec{u} \cdot \vec{v}}{\|\vec{u}\|\|\vec{v}\|} = \frac{4}{(3)(3)} = \frac{4}{9} \implies \theta = \arccos\left(\frac{4}{9}\right) \approx 63.61^\circcosΞΈ=βˆ₯uβˆ₯βˆ₯vβˆ₯uβ‹…v​=(3)(3)4​=94β€‹βŸΉΞΈ=arccos(94​)β‰ˆ63.61∘

  2. Calculate Scalar and Vector Projections: State the Scalar Projection Formula:

    scaluβƒ—vβƒ—=uβƒ—β‹…vβƒ—βˆ₯uβƒ—βˆ₯=43\text{scal}_{\vec{u}}\vec{v} = \frac{\vec{u} \cdot \vec{v}}{\|\vec{u}\|} = \frac{4}{3}scalu​v=βˆ₯uβˆ₯uβ‹…v​=34​

    State the Vector Projection Formula:

    projuβƒ—vβƒ—=(uβƒ—β‹…vβƒ—βˆ₯uβƒ—βˆ₯2)uβƒ—=49⟨2,βˆ’1,2⟩=⟨89,βˆ’49,89⟩\text{proj}_{\vec{u}}\vec{v} = \left( \frac{\vec{u} \cdot \vec{v}}{\|\vec{u}\|^2} \right) \vec{u} = \frac{4}{9}\langle 2, -1, 2 \rangle = \left\langle \frac{8}{9}, -\frac{4}{9}, \frac{8}{9} \right\rangleproju​v=(βˆ₯uβˆ₯2uβ‹…v​)u=94β€‹βŸ¨2,βˆ’1,2⟩=⟨98​,βˆ’94​,98β€‹βŸ©
    (Defined in Vector Projections.)

  3. Compute and Verify the Orthogonal Component: State the Orthogonal Component Formula:

    orthuβƒ—vβƒ—=vβƒ—βˆ’projuβƒ—vβƒ—=⟨1,2,2βŸ©βˆ’βŸ¨89,βˆ’49,89⟩=⟨9βˆ’89,18βˆ’(βˆ’4)9,18βˆ’89⟩=⟨19,229,109⟩\text{orth}_{\vec{u}}\vec{v} = \vec{v} - \text{proj}_{\vec{u}}\vec{v} = \langle 1, 2, 2 \rangle - \left\langle \frac{8}{9}, -\frac{4}{9}, \frac{8}{9} \right\rangle = \left\langle \frac{9 - 8}{9}, \frac{18 - (-4)}{9}, \frac{18 - 8}{9} \right\rangle = \left\langle \frac{1}{9}, \frac{22}{9}, \frac{10}{9} \right\rangleorthu​v=vβˆ’proju​v=⟨1,2,2βŸ©βˆ’βŸ¨98​,βˆ’94​,98β€‹βŸ©=⟨99βˆ’8​,918βˆ’(βˆ’4)​,918βˆ’8β€‹βŸ©=⟨91​,922​,910β€‹βŸ©

    Verify orthogonality:

    orthuβƒ—vβƒ—β‹…uβƒ—=(19)(2)+(229)(βˆ’1)+(109)(2)=2βˆ’22+209=09=0βœ“\text{orth}_{\vec{u}}\vec{v} \cdot \vec{u} = \left(\frac{1}{9}\right)(2) + \left(\frac{22}{9}\right)(-1) + \left(\frac{10}{9}\right)(2) = \frac{2 - 22 + 20}{9} = \frac{0}{9} = 0\quad \checkmarkorthu​vβ‹…u=(91​)(2)+(922​)(βˆ’1)+(910​)(2)=92βˆ’22+20​=90​=0βœ“

  4. Compute Cross Product and Parallelogram Area: State the Cross Product Determinant Formula:

    uβƒ—Γ—vβƒ—=∣i^j^k^2βˆ’12122∣\vec{u} \times \vec{v} = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 2 & -1 & 2 \\ 1 & 2 & 2 \end{vmatrix}uΓ—v=​i^21​j^β€‹βˆ’12​k^22​​
    (Defined in Cross Product.)

    uβƒ—Γ—vβƒ—=⟨(βˆ’1)(2)βˆ’(2)(2),β€…β€Š(2)(1)βˆ’(2)(2),β€…β€Š(2)(2)βˆ’(βˆ’1)(1)⟩=βŸ¨βˆ’2βˆ’4,β€…β€Š2βˆ’4,β€…β€Š4+1⟩=βŸ¨βˆ’6,βˆ’2,5⟩\vec{u} \times \vec{v} = \langle (-1)(2) - (2)(2), \; (2)(1) - (2)(2), \; (2)(2) - (-1)(1) \rangle = \langle -2 - 4, \; 2 - 4, \; 4 + 1 \rangle = \langle -6, -2, 5 \rangleuΓ—v=⟨(βˆ’1)(2)βˆ’(2)(2),(2)(1)βˆ’(2)(2),(2)(2)βˆ’(βˆ’1)(1)⟩=βŸ¨βˆ’2βˆ’4,2βˆ’4,4+1⟩=βŸ¨βˆ’6,βˆ’2,5⟩

    Area of Parallelogram:

    Area=βˆ₯uβƒ—Γ—vβƒ—βˆ₯=(βˆ’6)2+(βˆ’2)2+52=36+4+25=65Β units2\text{Area} = \|\vec{u} \times \vec{v}\| = \sqrt{(-6)^2 + (-2)^2 + 5^2} = \sqrt{36 + 4 + 25} = \sqrt{65}\text{ units}^2Area=βˆ₯uΓ—vβˆ₯=(βˆ’6)2+(βˆ’2)2+52​=36+4+25​=65​ units2

Practice Problem 1: Concept & Reading Check

Open this Skill Block on the Memex to locate the information needed to answer the following:

  • (a) Explain the geometric and dimensional difference between the scalar projection scaluβƒ—vβƒ—\text{scal}_{\vec{u}}\vec{v}scalu​v and the vector projection projuβƒ—vβƒ—\text{proj}_{\vec{u}}\vec{v}proju​v.
  • (b) In Worked Example A step 3, state the mathematical definition of orthogonality and show how the dot product proves perpendicularity.
  • (c) In Suspension Bridge Guy-Wire Force Decomposition (Civil & Mechanical Engineering), why is the overturning moment torque about the tower base zero?
Solution Key:
  • (a) Scalar vs Vector Projection: The scalar projection scaluβƒ—vβƒ—=uβƒ—β‹…vβƒ—βˆ₯uβƒ—βˆ₯\text{scal}_{\vec{u}}\vec{v} = \frac{\vec{u}\cdot\vec{v}}{\|\vec{u}\|}scalu​v=βˆ₯uβˆ₯uβ‹…v​ represents the signed scalar length of the shadow cast by vβƒ—\vec{v}v onto the axis spanned by uβƒ—\vec{u}u. The vector projection projuβƒ—vβƒ—=(scaluβƒ—vβƒ—)u^=(uβƒ—β‹…vβƒ—βˆ₯uβƒ—βˆ₯2)uβƒ—\text{proj}_{\vec{u}}\vec{v} = (\text{scal}_{\vec{u}}\vec{v})\hat{u} = \left(\frac{\vec{u}\cdot\vec{v}}{\|\vec{u}\|^2}\right)\vec{u}proju​v=(scalu​v)u^=(βˆ₯uβˆ₯2uβ‹…v​)u scales the unit direction vector u^\hat{u}u^ by this scalar length, producing a true vector in R3\mathbb{R}^3R3.
  • (b) Orthogonality Condition: Two non-zero vectors aβƒ—\vec{a}a and bβƒ—\vec{b}b are perpendicular if the angle between them is ΞΈ=90∘\theta = 90^\circΞΈ=90∘. Since cos⁑(90∘)=0\cos(90^\circ) = 0cos(90∘)=0, the governing equation is aβƒ—β‹…bβƒ—=βˆ₯aβƒ—βˆ₯βˆ₯bβƒ—βˆ₯cos⁑(90∘)=0\vec{a} \cdot \vec{b} = \|\vec{a}\|\|\vec{b}\|\cos(90^\circ) = 0aβ‹…b=βˆ₯aβˆ₯βˆ₯bβˆ₯cos(90∘)=0. In step 3, computing (orthuβƒ—vβƒ—)β‹…uβƒ—=0(\text{orth}_{\vec{u}}\vec{v}) \cdot \vec{u} = 0(orthu​v)β‹…u=0 confirms that the residual vector is strictly perpendicular to uβƒ—\vec{u}u.
  • (c) Zero Overturning Moment: Torque is defined by the cross product Ο„βƒ—=rβƒ—Γ—Fβƒ—=βˆ₯rβƒ—βˆ₯βˆ₯Fβƒ—βˆ₯sin⁑θn^\vec{\tau} = \vec{r} \times \vec{F} = \|\vec{r}\|\|\vec{F}\|\sin\theta \hat{n}Ο„=rΓ—F=βˆ₯rβˆ₯βˆ₯Fβˆ₯sinΞΈn^. When the force vector acts directly along the line of the position vector, the angle is ΞΈ=0∘\theta = 0^\circΞΈ=0∘ (or 180∘180^\circ180∘). Because sin⁑(0∘)=0\sin(0^\circ) = 0sin(0∘)=0, the cross product vanishes (rβƒ—Γ—Fβƒ—=0βƒ—\vec{r} \times \vec{F} = \vec{0}rΓ—F=0), producing zero overturning moment about the footing.
Show your steps and calculations here.

Practice Problem 2

Given points A(1,1,0)A(1, 1, 0)A(1,1,0), B(3,2,2)B(3, 2, 2)B(3,2,2), and C(1,4,0)C(1, 4, 0)C(1,4,0) in R3\mathbb{R}^3R3:

  1. Determine the displacement vectors AB⃗\vec{AB}AB and AC⃗\vec{AC}AC in component form.
  2. Decompose ABβƒ—\vec{AB}AB into a vector component parallel to ACβƒ—\vec{AC}AC (projACβƒ—ABβƒ—\text{proj}_{\vec{AC}}\vec{AB}projAC​AB) and a component perpendicular to ACβƒ—\vec{AC}AC (orthACβƒ—ABβƒ—\text{orth}_{\vec{AC}}\vec{AB}orthAC​AB).
  3. Calculate the exact area of triangle β–³ABC\triangle ABCβ–³ABC.
Solution Key:
  1. Find Displacement Vectors: State the Displacement Vector Formula:

    ABβƒ—=⟨xBβˆ’xA,β€…β€ŠyBβˆ’yA,β€…β€ŠzBβˆ’zA⟩=⟨3βˆ’1,β€…β€Š2βˆ’1,β€…β€Š2βˆ’0⟩=⟨2,1,2⟩\vec{AB} = \langle x_B - x_A, \; y_B - y_A, \; z_B - z_A \rangle = \langle 3 - 1, \; 2 - 1, \; 2 - 0 \rangle = \langle 2, 1, 2 \rangleAB=⟨xBβ€‹βˆ’xA​,yBβ€‹βˆ’yA​,zBβ€‹βˆ’zAβ€‹βŸ©=⟨3βˆ’1,2βˆ’1,2βˆ’0⟩=⟨2,1,2⟩
    ACβƒ—=⟨xCβˆ’xA,β€…β€ŠyCβˆ’yA,β€…β€ŠzCβˆ’zA⟩=⟨1βˆ’1,β€…β€Š4βˆ’1,β€…β€Š0βˆ’0⟩=⟨0,3,0⟩\vec{AC} = \langle x_C - x_A, \; y_C - y_A, \; z_C - z_A \rangle = \langle 1 - 1, \; 4 - 1, \; 0 - 0 \rangle = \langle 0, 3, 0 \rangleAC=⟨xCβ€‹βˆ’xA​,yCβ€‹βˆ’yA​,zCβ€‹βˆ’zAβ€‹βŸ©=⟨1βˆ’1,4βˆ’1,0βˆ’0⟩=⟨0,3,0⟩

  2. Compute Projections: State the Dot Product and Magnitude:

    AB⃗⋅AC⃗=(2)(0)+(1)(3)+(2)(0)=3\vec{AB} \cdot \vec{AC} = (2)(0) + (1)(3) + (2)(0) = 3AB⋅AC=(2)(0)+(1)(3)+(2)(0)=3
    βˆ₯ACβƒ—βˆ₯2=02+32+02=9\|\vec{AC}\|^2 = 0^2 + 3^2 + 0^2 = 9βˆ₯ACβˆ₯2=02+32+02=9

    State the Vector Projection Formula:

    projACβƒ—ABβƒ—=(ABβƒ—β‹…ACβƒ—βˆ₯ACβƒ—βˆ₯2)ACβƒ—=39⟨0,3,0⟩=13⟨0,3,0⟩=⟨0,1,0⟩\text{proj}_{\vec{AC}}\vec{AB} = \left( \frac{\vec{AB} \cdot \vec{AC}}{\|\vec{AC}\|^2} \right) \vec{AC} = \frac{3}{9}\langle 0, 3, 0 \rangle = \frac{1}{3}\langle 0, 3, 0 \rangle = \langle 0, 1, 0 \rangleprojAC​AB=(βˆ₯ACβˆ₯2ABβ‹…AC​)AC=93β€‹βŸ¨0,3,0⟩=31β€‹βŸ¨0,3,0⟩=⟨0,1,0⟩

    State the Orthogonal Component Formula:

    orthACβƒ—ABβƒ—=ABβƒ—βˆ’projACβƒ—ABβƒ—=⟨2,1,2βŸ©βˆ’βŸ¨0,1,0⟩=⟨2,0,2⟩\text{orth}_{\vec{AC}}\vec{AB} = \vec{AB} - \text{proj}_{\vec{AC}}\vec{AB} = \langle 2, 1, 2 \rangle - \langle 0, 1, 0 \rangle = \langle 2, 0, 2 \rangleorthAC​AB=ABβˆ’projAC​AB=⟨2,1,2βŸ©βˆ’βŸ¨0,1,0⟩=⟨2,0,2⟩
    (Notice that ⟨2,0,2βŸ©β‹…βŸ¨0,3,0⟩=0\langle 2, 0, 2 \rangle \cdot \langle 0, 3, 0 \rangle = 0⟨2,0,2βŸ©β‹…βŸ¨0,3,0⟩=0, confirming orthogonality).

  3. Compute Triangle Area: State the Cross Product Formula:

    ABβƒ—Γ—ACβƒ—=∣i^j^k^212030∣=⟨(1)(0)βˆ’(2)(3),β€…β€Š(2)(0)βˆ’(2)(0),β€…β€Š(2)(3)βˆ’(1)(0)⟩=βŸ¨βˆ’6,0,6⟩\vec{AB} \times \vec{AC} = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 2 & 1 & 2 \\ 0 & 3 & 0 \\ \end{vmatrix} = \langle (1)(0) - (2)(3), \; (2)(0) - (2)(0), \; (2)(3) - (1)(0) \rangle = \langle -6, 0, 6 \rangleABΓ—AC=​i^20​j^​13​k^20​​=⟨(1)(0)βˆ’(2)(3),(2)(0)βˆ’(2)(0),(2)(3)βˆ’(1)(0)⟩=βŸ¨βˆ’6,0,6⟩

    State the Triangle Area Formula:

    Area(β–³ABC)=12βˆ₯ABβƒ—Γ—ACβƒ—βˆ₯=12(βˆ’6)2+02+62=1236+36=1272=12(62)=32Β units2\text{Area}(\triangle ABC) = \frac{1}{2}\|\vec{AB} \times \vec{AC}\| = \frac{1}{2}\sqrt{(-6)^2 + 0^2 + 6^2} = \frac{1}{2}\sqrt{36 + 36} = \frac{1}{2}\sqrt{72} = \frac{1}{2}(6\sqrt{2}) = 3\sqrt{2}\text{ units}^2Area(β–³ABC)=21​βˆ₯ABΓ—ACβˆ₯=21​(βˆ’6)2+02+62​=21​36+36​=21​72​=21​(62​)=32​ units2

Show your steps and calculations here.

Practice Problem 3

Given vectors uβƒ—=⟨2,1,0⟩\vec{u} = \langle 2, 1, 0 \rangleu=⟨2,1,0⟩, vβƒ—=⟨1,3,βˆ’1⟩\vec{v} = \langle 1, 3, -1 \ranglev=⟨1,3,βˆ’1⟩, and wβƒ—=⟨0,2,4⟩\vec{w} = \langle 0, 2, 4 \ranglew=⟨0,2,4⟩ in R3\mathbb{R}^3R3:

  1. Compute the cross product v⃗×w⃗\vec{v} \times \vec{w}v×w.
  2. Compute the triple scalar product u⃗⋅(v⃗×w⃗)\vec{u} \cdot (\vec{v} \times \vec{w})u⋅(v×w).
  3. Determine the volume of the parallelepiped spanned by u⃗,v⃗,w⃗\vec{u}, \vec{v}, \vec{w}u,v,w, and state whether the three vectors are coplanar.
Solution Key:
  1. Compute Cross Product v⃗×w⃗\vec{v} \times \vec{w}v×w: State the Cross Product Determinant Formula:

    vβƒ—Γ—wβƒ—=∣i^j^k^13βˆ’1024∣=⟨(3)(4)βˆ’(βˆ’1)(2),β€…β€Š(βˆ’1)(0)βˆ’(1)(4),β€…β€Š(1)(2)βˆ’(3)(0)⟩=⟨14,βˆ’4,2⟩\vec{v} \times \vec{w} = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 1 & 3 & -1 \\ 0 & 2 & 4 \end{vmatrix} = \langle (3)(4) - (-1)(2), \; (-1)(0) - (1)(4), \; (1)(2) - (3)(0) \rangle = \langle 14, -4, 2 \ranglevΓ—w=​i^10​j^​32​k^βˆ’14​​=⟨(3)(4)βˆ’(βˆ’1)(2),(βˆ’1)(0)βˆ’(1)(4),(1)(2)βˆ’(3)(0)⟩=⟨14,βˆ’4,2⟩

  2. Compute Triple Scalar Product: State the Triple Scalar Product Formula:

    uβƒ—β‹…(vβƒ—Γ—wβƒ—)=⟨2,1,0βŸ©β‹…βŸ¨14,βˆ’4,2⟩=(2)(14)+(1)(βˆ’4)+(0)(2)=28βˆ’4+0=24\vec{u} \cdot (\vec{v} \times \vec{w}) = \langle 2, 1, 0 \rangle \cdot \langle 14, -4, 2 \rangle = (2)(14) + (1)(-4) + (0)(2) = 28 - 4 + 0 = 24uβ‹…(vΓ—w)=⟨2,1,0βŸ©β‹…βŸ¨14,βˆ’4,2⟩=(2)(14)+(1)(βˆ’4)+(0)(2)=28βˆ’4+0=24
    (Defined in Triple Scalar Product and Spatial Volume.)

  3. Determine Volume and Test Coplanarity: State the Parallelepiped Volume Formula:

    Volume=∣uβƒ—β‹…(vβƒ—Γ—wβƒ—)∣=∣24∣=24Β units3\text{Volume} = |\vec{u} \cdot (\vec{v} \times \vec{w})| = |24| = 24\text{ units}^3Volume=∣uβ‹…(vΓ—w)∣=∣24∣=24Β units3
    Because the triple scalar product evaluates to a non-zero value (24β‰ 024 \ne 024ξ€ =0), the three vectors span a three-dimensional volume and are not coplanar.


Show your steps and calculations here.

Regroup 1

  • Projection Direction Trap: projuβƒ—vβƒ—\text{proj}_{\vec{u}}\vec{v}proju​v points strictly along vector uβƒ—\vec{u}u, NOT vβƒ—\vec{v}v. Always divide by βˆ₯uβƒ—βˆ₯2\|\vec{u}\|^2βˆ₯uβˆ₯2 and multiply by vector uβƒ—\vec{u}u.
  • Cross Product Non-Commutativity: uβƒ—Γ—vβƒ—=βˆ’(vβƒ—Γ—uβƒ—)\vec{u} \times \vec{v} = -(\vec{v} \times \vec{u})uΓ—v=βˆ’(vΓ—u). Order matters for direction, though magnitude (area) is preserved.

Skill Block 2

Worked Example A: Classifying 3D Lines and Computing Shortest Clearances

Consider line L1L_1L1​ passing through point P(1,0,2)P(1, 0, 2)P(1,0,2) with direction vector vβƒ—1=⟨2,1,βˆ’1⟩\vec{v}_1 = \langle 2, 1, -1 \ranglev1​=⟨2,1,βˆ’1⟩, and line L2L_2L2​ passing through point Q(0,3,1)Q(0, 3, 1)Q(0,3,1) with direction vector vβƒ—2=⟨1,βˆ’1,2⟩\vec{v}_2 = \langle 1, -1, 2 \ranglev2​=⟨1,βˆ’1,2⟩.

  1. Write the vector and parametric equations for L1L_1L1​ (parameter ttt) and L2L_2L2​ (parameter sss).
  2. Classify the geometric relationship between L1L_1L1​ and L2L_2L2​ (Parallel, Intersecting, Skew, or Coincident).
  3. Compute the shortest perpendicular distance from point P(1,0,2)P(1, 0, 2)P(1,0,2) on L1L_1L1​ to line L2L_2L2​.
Worked Solution:
  1. Formulate Equations of Lines: State the Vector Equation of a Line Formula:

    rβƒ—(t)=rβƒ—0+tvβƒ—\vec{r}(t) = \vec{r}_0 + t\vec{v}r(t)=r0​+tv
    (Defined in Equations of Lines in 3D.)

    • Line L1L_1L1​: rβƒ—1(t)=⟨1+2t,β€…β€Št,β€…β€Š2βˆ’t⟩\vec{r}_1(t) = \langle 1 + 2t, \; t, \; 2 - t \rangler1​(t)=⟨1+2t,t,2βˆ’t⟩
      Parametric:Β x1=1+2t,y1=t,z1=2βˆ’t\text{Parametric: } x_1 = 1 + 2t, \quad y_1 = t, \quad z_1 = 2 - tParametric:Β x1​=1+2t,y1​=t,z1​=2βˆ’t
    • Line L2L_2L2​: rβƒ—2(s)=⟨s,β€…β€Š3βˆ’s,β€…β€Š1+2s⟩\vec{r}_2(s) = \langle s, \; 3 - s, \; 1 + 2s \rangler2​(s)=⟨s,3βˆ’s,1+2s⟩
      Parametric:Β x2=s,y2=3βˆ’s,z2=1+2s\text{Parametric: } x_2 = s, \quad y_2 = 3 - s, \quad z_2 = 1 + 2sParametric:Β x2​=s,y2​=3βˆ’s,z2​=1+2s
  2. Classify the Spatial Relationship: State the Line Classification Protocol: (Defined in Relationships Between Lines in Space.)

    • Parallel Check: Compare direction vectors:
      vβƒ—1=⟨2,1,βˆ’1⟩,vβƒ—2=⟨1,βˆ’1,2⟩\vec{v}_1 = \langle 2, 1, -1 \rangle, \quad \vec{v}_2 = \langle 1, -1, 2 \ranglev1​=⟨2,1,βˆ’1⟩,v2​=⟨1,βˆ’1,2⟩
      21β‰ 1βˆ’1β€…β€ŠβŸΉβ€…β€Švβƒ—1β‰ kvβƒ—2(NotΒ Parallel)\frac{2}{1} \ne \frac{1}{-1} \implies \vec{v}_1 \ne k\vec{v}_2 \quad (\text{Not Parallel})12​=βˆ’11β€‹βŸΉv1​=kv2​(NotΒ Parallel)
    • Intersection Check: Set rβƒ—1(t)=rβƒ—2(s)\vec{r}_1(t) = \vec{r}_2(s)r1​(t)=r2​(s):
      {1+2t=s(1)t=3βˆ’s(2)2βˆ’t=1+2s(3)\begin{cases} 1 + 2t = s & (1) \\ t = 3 - s & (2) \\ 2 - t = 1 + 2s & (3) \end{cases}βŽ©βŽ¨βŽ§β€‹1+2t=st=3βˆ’s2βˆ’t=1+2s​(1)(2)(3)​
      Substitute (1) into (2):
      t=3βˆ’(1+2t)=2βˆ’2tβ€…β€ŠβŸΉβ€…β€Š3t=2β€…β€ŠβŸΉβ€…β€Št=23t = 3 - (1 + 2t) = 2 - 2t \implies 3t = 2 \implies t = \frac{2}{3}t=3βˆ’(1+2t)=2βˆ’2t⟹3t=2⟹t=32​
      Then from (1): s=1+2(23)=73s = 1 + 2\left(\frac{2}{3}\right) = \frac{7}{3}s=1+2(32​)=37​. Test (t=23,s=73)\left(t = \frac{2}{3}, s = \frac{7}{3}\right)(t=32​,s=37​) in equation (3):
      LHS=2βˆ’23=43\text{LHS} = 2 - \frac{2}{3} = \frac{4}{3}LHS=2βˆ’32​=34​
      RHS=1+2(73)=1+143=173\text{RHS} = 1 + 2\left(\frac{7}{3}\right) = 1 + \frac{14}{3} = \frac{17}{3}RHS=1+2(37​)=1+314​=317​
      43β‰ 173(Inconsistent)\frac{4}{3} \ne \frac{17}{3} \quad (\text{Inconsistent})34​=317​(Inconsistent)
    • Classification: Because the direction vectors are non-parallel and the linear system has no solution, lines L1L_1L1​ and L2L_2L2​ are Skew.
  3. Compute Perpendicular Distance from P(1,0,2)P(1, 0, 2)P(1,0,2) to Line L2L_2L2​: State the Point-to-Line Distance Formula:

    d=βˆ₯QPβƒ—Γ—vβƒ—2βˆ₯βˆ₯vβƒ—2βˆ₯d = \frac{\|\vec{QP} \times \vec{v}_2\|}{\|\vec{v}_2\|}d=βˆ₯v2​βˆ₯βˆ₯QP​×v2​βˆ₯​
    (Defined in Distance Between a Point and a Line in Space.)

    1. Find displacement vector QPβƒ—\vec{QP}QP​ from Q(0,3,1)Q(0, 3, 1)Q(0,3,1) to P(1,0,2)P(1, 0, 2)P(1,0,2):
      QPβƒ—=⟨1βˆ’0,β€…β€Š0βˆ’3,β€…β€Š2βˆ’1⟩=⟨1,βˆ’3,1⟩\vec{QP} = \langle 1 - 0, \; 0 - 3, \; 2 - 1 \rangle = \langle 1, -3, 1 \rangleQP​=⟨1βˆ’0,0βˆ’3,2βˆ’1⟩=⟨1,βˆ’3,1⟩
    2. Compute cross product QPβƒ—Γ—vβƒ—2\vec{QP} \times \vec{v}_2QP​×v2​:
      QPβƒ—Γ—vβƒ—2=∣i^j^k^1βˆ’311βˆ’12∣=⟨(βˆ’3)(2)βˆ’(1)(βˆ’1),β€…β€Š(1)(1)βˆ’(1)(2),β€…β€Š(1)(βˆ’1)βˆ’(βˆ’3)(1)⟩\vec{QP} \times \vec{v}_2 = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 1 & -3 & 1 \\ 1 & -1 & 2 \end{vmatrix} = \langle (-3)(2) - (1)(-1), \; (1)(1) - (1)(2), \; (1)(-1) - (-3)(1) \rangleQP​×v2​=​i^11​j^β€‹βˆ’3βˆ’1​k^12​​=⟨(βˆ’3)(2)βˆ’(1)(βˆ’1),(1)(1)βˆ’(1)(2),(1)(βˆ’1)βˆ’(βˆ’3)(1)⟩
      QPβƒ—Γ—vβƒ—2=βŸ¨βˆ’6+1,β€…β€Š1βˆ’2,β€…β€Šβˆ’1+3⟩=βŸ¨βˆ’5,βˆ’1,2⟩\vec{QP} \times \vec{v}_2 = \langle -6 + 1, \; 1 - 2, \; -1 + 3 \rangle = \langle -5, -1, 2 \rangleQP​×v2​=βŸ¨βˆ’6+1,1βˆ’2,βˆ’1+3⟩=βŸ¨βˆ’5,βˆ’1,2⟩
    3. Compute magnitudes:
      βˆ₯QPβƒ—Γ—vβƒ—2βˆ₯=(βˆ’5)2+(βˆ’1)2+22=25+1+4=30\|\vec{QP} \times \vec{v}_2\| = \sqrt{(-5)^2 + (-1)^2 + 2^2} = \sqrt{25 + 1 + 4} = \sqrt{30}βˆ₯QP​×v2​βˆ₯=(βˆ’5)2+(βˆ’1)2+22​=25+1+4​=30​
      βˆ₯vβƒ—2βˆ₯=12+(βˆ’1)2+22=1+1+4=6\|\vec{v}_2\| = \sqrt{1^2 + (-1)^2 + 2^2} = \sqrt{1 + 1 + 4} = \sqrt{6}βˆ₯v2​βˆ₯=12+(βˆ’1)2+22​=1+1+4​=6​
    4. Calculate exact distance:
      d=306=306=5Β unitsd = \frac{\sqrt{30}}{\sqrt{6}} = \sqrt{\frac{30}{6}} = \sqrt{5}\text{ units}d=6​30​​=630​​=5​ units

Practice Problem 4: Concept & Reading Check

Open this Skill Block on the Memex to locate the information needed to answer the following:

  • (a) Why must you use two distinct parameters (ttt and sss) when testing whether two lines in 3D space intersect?
  • (b) Deconstruct Worked Example A step 2: what algebraic outcome confirms that lines are skew rather than parallel or intersecting?
  • (c) In Autonomous Drone Flight Path Separation (Aerospace & Computer Engineering), what geometric threshold determines whether an emergency avoidance maneuver is required?
Solution Key:
  • (a) Parameter Decoupling: In physical kinematics, the parameter ttt often represents time. If you use the same parameter ttt for both lines, setting rβƒ—1(t)=rβƒ—2(t)\vec{r}_1(t) = \vec{r}_2(t)r1​(t)=r2​(t) only tests whether the two objects will collide at the exact same instant. Two physical paths can cross at the same spatial coordinates (x,y,z)(x,y,z)(x,y,z) at completely different times (tβ‰ st \ne stξ€ =s). Using independent parameters ttt and sss tests for true geometric intersection of the curves.
  • (b) Skew Line Criteria: Skew lines are defined as lines in R3\mathbb{R}^3R3 that are non-coplanar, which requires two distinct conditions: (1) their direction vectors are non-parallel (vβƒ—1β‰ kvβƒ—2\vec{v}_1 \ne k\vec{v}_2v1​=kv2​), and (2) their paths do not intersect, proven algebraically when the (t,s)(t, s)(t,s) values obtained from two coordinate equations fail to satisfy the third coordinate equation.
  • (c) Clearance Threshold: In the autonomous drone scenario, the FAA clearance standard mandates that the minimum perpendicular distance between the drone's position and the neighboring flight path corridor must satisfy dβ‰₯2.0Β md \ge 2.0\text{ m}dβ‰₯2.0Β m. Computing d=2.89Β mβ‰₯2.0Β md = 2.89\text{ m} \ge 2.0\text{ m}d=2.89Β mβ‰₯2.0Β m confirms compliance without requiring an emergency trajectory override.
Show your steps and calculations here.

Practice Problem 5

Line L1L_1L1​ is given by symmetric equations xβˆ’21=y+12=zβˆ’31\frac{x-2}{1} = \frac{y+1}{2} = \frac{z-3}{1}1xβˆ’2​=2y+1​=1zβˆ’3​, and line L2L_2L2​ is given by parametric equations x=1+2sx = 1 + 2sx=1+2s, y=3+4sy = 3 + 4sy=3+4s, z=2+2sz = 2 + 2sz=2+2s.

  1. Extract direction vectors vβƒ—1\vec{v}_1v1​ and vβƒ—2\vec{v}_2v2​ and determine whether the lines are parallel.
  2. Determine whether L1L_1L1​ and L2L_2L2​ are coincident (the same line) or distinct parallel lines.
  3. Compute the shortest perpendicular distance between the two parallel lines.
Solution Key:
  1. Extract Direction Vectors and Test Parallelism:

    • From symmetric equations of L1L_1L1​: reference point P(2,βˆ’1,3)P(2, -1, 3)P(2,βˆ’1,3) and direction vector vβƒ—1=⟨1,2,1⟩\vec{v}_1 = \langle 1, 2, 1 \ranglev1​=⟨1,2,1⟩.
    • From parametric equations of L2L_2L2​: reference point Q(1,3,2)Q(1, 3, 2)Q(1,3,2) and direction vector vβƒ—2=⟨2,4,2⟩\vec{v}_2 = \langle 2, 4, 2 \ranglev2​=⟨2,4,2⟩.
    • Proportionality check:
      vβƒ—2=⟨2,4,2⟩=2⟨1,2,1⟩=2vβƒ—1\vec{v}_2 = \langle 2, 4, 2 \rangle = 2\langle 1, 2, 1 \rangle = 2\vec{v}_1v2​=⟨2,4,2⟩=2⟨1,2,1⟩=2v1​
      Because vβƒ—2=2vβƒ—1\vec{v}_2 = 2\vec{v}_1v2​=2v1​, lines L1L_1L1​ and L2L_2L2​ are Parallel.
  2. Test for Coincidence: Test whether point P(2,βˆ’1,3)∈P(2, -1, 3) \inP(2,βˆ’1,3)∈ line L1L_1L1​ lies on line L2L_2L2​:

    x:1+2s=2β€…β€ŠβŸΉβ€…β€Š2s=1β€…β€ŠβŸΉβ€…β€Šs=12x: 1 + 2s = 2 \implies 2s = 1 \implies s = \frac{1}{2}x:1+2s=2⟹2s=1⟹s=21​
    Test s=1/2s = 1/2s=1/2 in the yyy-equation of L2L_2L2​:
    y(12)=3+4(12)=3+2=5β‰ βˆ’1y\left(\frac{1}{2}\right) = 3 + 4\left(\frac{1}{2}\right) = 3 + 2 = 5 \ne -1y(21​)=3+4(21​)=3+2=5ξ€ =βˆ’1
    Since P(2,βˆ’1,3)P(2, -1, 3)P(2,βˆ’1,3) does not satisfy L2L_2L2​, the lines are Distinct Parallel Lines.

  3. Compute Perpendicular Distance between Parallel Lines: State the Point-to-Line Distance Formula:

    d=βˆ₯QPβƒ—Γ—vβƒ—1βˆ₯βˆ₯vβƒ—1βˆ₯d = \frac{\|\vec{QP} \times \vec{v}_1\|}{\|\vec{v}_1\|}d=βˆ₯v1​βˆ₯βˆ₯QP​×v1​βˆ₯​
    (Defined in Distance Between a Point and a Line in Space.)

    1. Find displacement vector QPβƒ—\vec{QP}QP​ from Q(1,3,2)Q(1, 3, 2)Q(1,3,2) to P(2,βˆ’1,3)P(2, -1, 3)P(2,βˆ’1,3):
      QPβƒ—=⟨2βˆ’1,β€…β€Šβˆ’1βˆ’3,β€…β€Š3βˆ’2⟩=⟨1,βˆ’4,1⟩\vec{QP} = \langle 2 - 1, \; -1 - 3, \; 3 - 2 \rangle = \langle 1, -4, 1 \rangleQP​=⟨2βˆ’1,βˆ’1βˆ’3,3βˆ’2⟩=⟨1,βˆ’4,1⟩
    2. Compute cross product QPβƒ—Γ—vβƒ—1\vec{QP} \times \vec{v}_1QP​×v1​:
      QPβƒ—Γ—vβƒ—1=∣i^j^k^1βˆ’41121∣=⟨(βˆ’4)(1)βˆ’(1)(2),β€…β€Š(1)(1)βˆ’(1)(1),β€…β€Š(1)(2)βˆ’(βˆ’4)(1)⟩\vec{QP} \times \vec{v}_1 = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 1 & -4 & 1 \\ 1 & 2 & 1 \end{vmatrix} = \langle (-4)(1) - (1)(2), \; (1)(1) - (1)(1), \; (1)(2) - (-4)(1) \rangleQP​×v1​=​i^11​j^β€‹βˆ’42​k^11​​=⟨(βˆ’4)(1)βˆ’(1)(2),(1)(1)βˆ’(1)(1),(1)(2)βˆ’(βˆ’4)(1)⟩
      QPβƒ—Γ—vβƒ—1=βŸ¨βˆ’4βˆ’2,β€…β€Š1βˆ’1,β€…β€Š2+4⟩=βŸ¨βˆ’6,0,6⟩\vec{QP} \times \vec{v}_1 = \langle -4 - 2, \; 1 - 1, \; 2 + 4 \rangle = \langle -6, 0, 6 \rangleQP​×v1​=βŸ¨βˆ’4βˆ’2,1βˆ’1,2+4⟩=βŸ¨βˆ’6,0,6⟩
    3. Compute magnitudes:
      βˆ₯QPβƒ—Γ—vβƒ—1βˆ₯=(βˆ’6)2+02+62=36+0+36=72=62\|\vec{QP} \times \vec{v}_1\| = \sqrt{(-6)^2 + 0^2 + 6^2} = \sqrt{36 + 0 + 36} = \sqrt{72} = 6\sqrt{2}βˆ₯QP​×v1​βˆ₯=(βˆ’6)2+02+62​=36+0+36​=72​=62​
      βˆ₯vβƒ—1βˆ₯=12+22+12=1+4+1=6\|\vec{v}_1\| = \sqrt{1^2 + 2^2 + 1^2} = \sqrt{1 + 4 + 1} = \sqrt{6}βˆ₯v1​βˆ₯=12+22+12​=1+4+1​=6​
    4. Calculate distance ddd:
      d=626=63=633=23Β unitsd = \frac{6\sqrt{2}}{\sqrt{6}} = \frac{6}{\sqrt{3}} = \frac{6\sqrt{3}}{3} = 2\sqrt{3}\text{ units}d=6​62​​=3​6​=363​​=23​ units
Show your steps and calculations here.

Practice Problem 6

Line L1L_1L1​ is given by rβƒ—1(t)=⟨1+2t,β€…β€Šβˆ’2+3t,β€…β€Š4βˆ’t⟩\vec{r}_1(t) = \langle 1 + 2t, \; -2 + 3t, \; 4 - t \rangler1​(t)=⟨1+2t,βˆ’2+3t,4βˆ’t⟩ and line L2L_2L2​ is given by rβƒ—2(s)=⟨1+s,β€…β€Š3βˆ’s,β€…β€Šβˆ’1+2s⟩\vec{r}_2(s) = \langle 1 + s, \; 3 - s, \; -1 + 2s \rangler2​(s)=⟨1+s,3βˆ’s,βˆ’1+2s⟩.

  1. Extract direction vectors vβƒ—1\vec{v}_1v1​ and vβƒ—2\vec{v}_2v2​ and verify that the lines are not parallel.
  2. Formulate the linear system rβƒ—1(t)=rβƒ—2(s)\vec{r}_1(t) = \vec{r}_2(s)r1​(t)=r2​(s) with independent parameters ttt and sss to classify the relationship (Intersecting or Skew). If the lines intersect, determine the exact point of intersection Pint(x,y,z)P_{\text{int}}(x, y, z)Pint​(x,y,z).
  3. Compute the shortest perpendicular distance from point Q(1,3,βˆ’1)Q(1, 3, -1)Q(1,3,βˆ’1) on L2L_2L2​ to line L1L_1L1​.
Solution Key:
  1. Verify Non-Parallel Direction Vectors:

    • Direction vector of L1L_1L1​: vβƒ—1=⟨2,3,βˆ’1⟩\vec{v}_1 = \langle 2, 3, -1 \ranglev1​=⟨2,3,βˆ’1⟩.
    • Direction vector of L2L_2L2​: vβƒ—2=⟨1,βˆ’1,2⟩\vec{v}_2 = \langle 1, -1, 2 \ranglev2​=⟨1,βˆ’1,2⟩. Because ⟨2,3,βˆ’1βŸ©β‰ k⟨1,βˆ’1,2⟩\langle 2, 3, -1 \rangle \ne k\langle 1, -1, 2 \rangle⟨2,3,βˆ’1βŸ©ξ€ =k⟨1,βˆ’1,2⟩, the direction vectors are not proportional, so L1L_1L1​ and L2L_2L2​ are not parallel.
  2. Formulate and Solve 2-Parameter Linear System: Set rβƒ—1(t)=rβƒ—2(s)\vec{r}_1(t) = \vec{r}_2(s)r1​(t)=r2​(s):

    {1+2t=1+s(EquationΒ 1)βˆ’2+3t=3βˆ’s(EquationΒ 2)4βˆ’t=βˆ’1+2s(EquationΒ 3)\begin{cases} 1 + 2t = 1 + s & \text{(Equation 1)} \\ -2 + 3t = 3 - s & \text{(Equation 2)} \\ 4 - t = -1 + 2s & \text{(Equation 3)} \end{cases}βŽ©βŽ¨βŽ§β€‹1+2t=1+sβˆ’2+3t=3βˆ’s4βˆ’t=βˆ’1+2s​(EquationΒ 1)(EquationΒ 2)(EquationΒ 3)​
    From Equation 1:
    s=2ts = 2ts=2t
    Substitute s=2ts = 2ts=2t into Equation 2:
    βˆ’2+3t=3βˆ’2tβ€…β€ŠβŸΉβ€…β€Š5t=5β€…β€ŠβŸΉβ€…β€Št=1-2 + 3t = 3 - 2t \implies 5t = 5 \implies t = 1βˆ’2+3t=3βˆ’2t⟹5t=5⟹t=1
    Then:
    s=2(1)=2s = 2(1) = 2s=2(1)=2
    Test (t=1,s=2)(t=1, s=2)(t=1,s=2) in Equation 3:
    LHS=4βˆ’(1)=3\text{LHS} = 4 - (1) = 3LHS=4βˆ’(1)=3
    RHS=βˆ’1+2(2)=βˆ’1+4=3\text{RHS} = -1 + 2(2) = -1 + 4 = 3RHS=βˆ’1+2(2)=βˆ’1+4=3
    Because LHS=RHS=3\text{LHS} = \text{RHS} = 3LHS=RHS=3, the system is strictly consistent. Therefore, the lines Intersect.

    Intersection Point:

    Pint=rβƒ—1(1)=⟨1+2(1),β€…β€Šβˆ’2+3(1),β€…β€Š4βˆ’1⟩=(3,1,3)P_{\text{int}} = \vec{r}_1(1) = \langle 1 + 2(1), \; -2 + 3(1), \; 4 - 1 \rangle = (3, 1, 3)Pint​=r1​(1)=⟨1+2(1),βˆ’2+3(1),4βˆ’1⟩=(3,1,3)

  3. Compute Perpendicular Clearance from Q(1,3,βˆ’1)Q(1, 3, -1)Q(1,3,βˆ’1) to L1L_1L1​: State the Point-to-Line Distance Formula:

    d=βˆ₯P1Qβƒ—Γ—vβƒ—1βˆ₯βˆ₯vβƒ—1βˆ₯d = \frac{\|\vec{P_1 Q} \times \vec{v}_1\|}{\|\vec{v}_1\|}d=βˆ₯v1​βˆ₯βˆ₯P1​Q​×v1​βˆ₯​
    Where P1(1,βˆ’2,4)P_1(1, -2, 4)P1​(1,βˆ’2,4) is the reference anchor point on L1L_1L1​:
    P1Qβƒ—=⟨1βˆ’1,β€…β€Š3βˆ’(βˆ’2),β€…β€Šβˆ’1βˆ’4⟩=⟨0,5,βˆ’5⟩\vec{P_1 Q} = \langle 1 - 1, \; 3 - (-2), \; -1 - 4 \rangle = \langle 0, 5, -5 \rangleP1​Q​=⟨1βˆ’1,3βˆ’(βˆ’2),βˆ’1βˆ’4⟩=⟨0,5,βˆ’5⟩
    Compute cross product P1Qβƒ—Γ—vβƒ—1\vec{P_1 Q} \times \vec{v}_1P1​Q​×v1​:
    P1Qβƒ—Γ—vβƒ—1=∣i^j^k^05βˆ’523βˆ’1∣=⟨(5)(βˆ’1)βˆ’(βˆ’5)(3),β€…β€Š(βˆ’5)(2)βˆ’(0)(βˆ’1),β€…β€Š(0)(3)βˆ’(5)(2)⟩\vec{P_1 Q} \times \vec{v}_1 = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ 0 & 5 & -5 \\ 2 & 3 & -1 \end{vmatrix} = \langle (5)(-1) - (-5)(3), \; (-5)(2) - (0)(-1), \; (0)(3) - (5)(2) \rangleP1​Q​×v1​=​i^02​j^​53​k^βˆ’5βˆ’1​​=⟨(5)(βˆ’1)βˆ’(βˆ’5)(3),(βˆ’5)(2)βˆ’(0)(βˆ’1),(0)(3)βˆ’(5)(2)⟩
    P1Qβƒ—Γ—vβƒ—1=βŸ¨βˆ’5+15,β€…β€Šβˆ’10βˆ’0,β€…β€Š0βˆ’10⟩=⟨10,βˆ’10,βˆ’10⟩\vec{P_1 Q} \times \vec{v}_1 = \langle -5 + 15, \; -10 - 0, \; 0 - 10 \rangle = \langle 10, -10, -10 \rangleP1​Q​×v1​=βŸ¨βˆ’5+15,βˆ’10βˆ’0,0βˆ’10⟩=⟨10,βˆ’10,βˆ’10⟩
    Compute magnitudes:
    βˆ₯P1Qβƒ—Γ—vβƒ—1βˆ₯=102+(βˆ’10)2+(βˆ’10)2=100+100+100=300=103\|\vec{P_1 Q} \times \vec{v}_1\| = \sqrt{10^2 + (-10)^2 + (-10)^2} = \sqrt{100 + 100 + 100} = \sqrt{300} = 10\sqrt{3}βˆ₯P1​Q​×v1​βˆ₯=102+(βˆ’10)2+(βˆ’10)2​=100+100+100​=300​=103​
    βˆ₯vβƒ—1βˆ₯=22+32+(βˆ’1)2=4+9+1=14\|\vec{v}_1\| = \sqrt{2^2 + 3^2 + (-1)^2} = \sqrt{4 + 9 + 1} = \sqrt{14}βˆ₯v1​βˆ₯=22+32+(βˆ’1)2​=4+9+1​=14​
    Calculate distance:
    d=10314=104214=5427Β unitsd = \frac{10\sqrt{3}}{\sqrt{14}} = \frac{10\sqrt{42}}{14} = \frac{5\sqrt{42}}{7}\text{ units}d=14​103​​=141042​​=7542​​ units


Show your steps and calculations here.

Regroup 2

  • The Skew Line Checklist: Remember that 3D lines are skew only when they are BOTH non-parallel AND non-intersecting. Always execute the direction vector proportionality test first before solving the linear system.
  • Symmetric Equation Conversion: If a symmetric component has a denominator of zero (e.g., xβˆ’12=yβˆ’34,z=5\frac{x-1}{2} = \frac{y-3}{4}, z = 52xβˆ’1​=4yβˆ’3​,z=5), the direction vector is vβƒ—=⟨2,4,0⟩\vec{v} = \langle 2, 4, 0 \ranglev=⟨2,4,0⟩.

Skill Block 3

Worked Example A: Space Curve Kinematics, Arc Length, Curvature, and Acceleration Decomposition

A high-speed test vehicle moves in R3\mathbb{R}^3R3 along the trajectory:

rβƒ—(t)=⟨3cos⁑t,β€…β€Š3sin⁑t,β€…β€Š4t⟩forΒ tβ‰₯0\vec{r}(t) = \langle 3\cos t, \; 3\sin t, \; 4t \rangle \quad \text{for } t \ge 0r(t)=⟨3cost,3sint,4t⟩forΒ tβ‰₯0

  1. Determine the velocity vβƒ—(t)\vec{v}(t)v(t), acceleration aβƒ—(t)\vec{a}(t)a(t), and scalar speed βˆ₯vβƒ—(t)βˆ₯\|\vec{v}(t)\|βˆ₯v(t)βˆ₯.
  2. Derive the accumulated arc length function s(t)s(t)s(t) starting at t=0t=0t=0, and construct the intrinsic arc length parametrization r⃗(s)\vec{r}(s)r(s).
  3. Compute the unit tangent vector T^(t)\hat{T}(t)T^(t) and curvature ΞΊ(t)\kappa(t)ΞΊ(t).
  4. Decompose the acceleration vector into tangential and normal components (aTa_TaT​ and aNa_NaN​).
Worked Solution:
  1. Compute Kinematics and Scalar Speed: State the Vector Derivative Formulas:

    vβƒ—(t)=rβƒ—β€²(t)=βŸ¨βˆ’3sin⁑t,β€…β€Š3cos⁑t,β€…β€Š4⟩\vec{v}(t) = \vec{r}'(t) = \langle -3\sin t, \; 3\cos t, \; 4 \ranglev(t)=rβ€²(t)=βŸ¨βˆ’3sint,3cost,4⟩
    aβƒ—(t)=rβƒ—β€²β€²(t)=βŸ¨βˆ’3cos⁑t,β€…β€Šβˆ’3sin⁑t,β€…β€Š0⟩\vec{a}(t) = \vec{r}''(t) = \langle -3\cos t, \; -3\sin t, \; 0 \ranglea(t)=rβ€²β€²(t)=βŸ¨βˆ’3cost,βˆ’3sint,0⟩
    (Defined in Derivatives of Vector-Valued Functions.)

    State the Scalar Speed Formula:

    βˆ₯vβƒ—(t)βˆ₯=(βˆ’3sin⁑t)2+(3cos⁑t)2+42=9(sin⁑2t+cos⁑2t)+16=9+16=25=5\|\vec{v}(t)\| = \sqrt{(-3\sin t)^2 + (3\cos t)^2 + 4^2} = \sqrt{9(\sin^2 t + \cos^2 t) + 16} = \sqrt{9 + 16} = \sqrt{25} = 5βˆ₯v(t)βˆ₯=(βˆ’3sint)2+(3cost)2+42​=9(sin2t+cos2t)+16​=9+16​=25​=5
    (The vehicle travels at a strictly constant speed of 5Β units/s5\text{ units/s}5Β units/s.)

  2. Derive s(t)s(t)s(t) and Parametrize by Arc Length r⃗(s)\vec{r}(s)r(s): State the Accumulated Arc Length Function Formula:

    s(t)=∫0tβˆ₯rβƒ—β€²(u)βˆ₯ du=∫0t5 du=[5u]0t=5ts(t) = \int_{0}^{t} \|\vec{r}'(u)\|\,du = \int_{0}^{t} 5\,du = [5u]_{0}^{t} = 5ts(t)=∫0t​βˆ₯rβ€²(u)βˆ₯du=∫0t​5du=[5u]0t​=5t
    (Defined in Arc Length of a Space Curve.)

    Invert s(t)s(t)s(t) to solve for ttt:

    s=5tβ€…β€ŠβŸΉβ€…β€Št(s)=s5s = 5t \implies t(s) = \frac{s}{5}s=5t⟹t(s)=5s​

    Substitute into r⃗(t)\vec{r}(t)r(t):

    rβƒ—(s)=⟨3cos⁑(s5),β€…β€Š3sin⁑(s5),β€…β€Š4(s5)⟩=⟨3cos⁑(s5),β€…β€Š3sin⁑(s5),β€…β€Š45s⟩\vec{r}(s) = \left\langle 3\cos\left(\frac{s}{5}\right), \; 3\sin\left(\frac{s}{5}\right), \; 4\left(\frac{s}{5}\right) \right\rangle = \left\langle 3\cos\left(\frac{s}{5}\right), \; 3\sin\left(\frac{s}{5}\right), \; \frac{4}{5}s \right\rangler(s)=⟨3cos(5s​),3sin(5s​),4(5s​)⟩=⟨3cos(5s​),3sin(5s​),54​s⟩
    (Notice that βˆ₯rβƒ—β€²(s)βˆ₯=(βˆ’3/5sin⁑)2+(3/5cos⁑)2+(4/5)2=9/25+16/25=1\|\vec{r}'(s)\| = \sqrt{(-3/5\sin)^2 + (3/5\cos)^2 + (4/5)^2} = \sqrt{9/25 + 16/25} = 1βˆ₯rβ€²(s)βˆ₯=(βˆ’3/5sin)2+(3/5cos)2+(4/5)2​=9/25+16/25​=1, confirming unit speed traversal as established in Arc Length Parametrization.)

  3. Compute Unit Tangent Vector T^(t)\hat{T}(t)T^(t) and Curvature ΞΊ(t)\kappa(t)ΞΊ(t): State the Unit Tangent Vector Formula:

    T^(t)=vβƒ—(t)βˆ₯vβƒ—(t)βˆ₯=15βŸ¨βˆ’3sin⁑t,β€…β€Š3cos⁑t,β€…β€Š4⟩=βŸ¨βˆ’35sin⁑t,β€…β€Š35cos⁑t,β€…β€Š45⟩\hat{T}(t) = \frac{\vec{v}(t)}{\|\vec{v}(t)\|} = \frac{1}{5}\langle -3\sin t, \; 3\cos t, \; 4 \rangle = \left\langle -\frac{3}{5}\sin t, \; \frac{3}{5}\cos t, \; \frac{4}{5} \right\rangleT^(t)=βˆ₯v(t)βˆ₯v(t)​=51β€‹βŸ¨βˆ’3sint,3cost,4⟩=βŸ¨βˆ’53​sint,53​cost,54β€‹βŸ©
    (Defined in Unit Tangent Vector.)

    State the Cross-Product Curvature Formula:

    ΞΊ=βˆ₯vβƒ—Γ—aβƒ—βˆ₯βˆ₯vβƒ—βˆ₯3\kappa = \frac{\|\vec{v} \times \vec{a}\|}{\|\vec{v}\|^3}ΞΊ=βˆ₯vβˆ₯3βˆ₯vΓ—aβˆ₯​
    (Defined in Curvature of a Space Curve.)

    Calculate v⃗×a⃗\vec{v} \times \vec{a}v×a:

    vβƒ—Γ—aβƒ—=∣i^j^k^βˆ’3sin⁑t3cos⁑t4βˆ’3cos⁑tβˆ’3sin⁑t0∣\vec{v} \times \vec{a} = \begin{vmatrix} \hat{i} & \hat{j} & \hat{k} \\ -3\sin t & 3\cos t & 4 \\ -3\cos t & -3\sin t & 0 \end{vmatrix}vΓ—a=​i^βˆ’3sintβˆ’3cost​j^​3costβˆ’3sint​k^40​​
    vβƒ—Γ—aβƒ—=⟨(3cos⁑t)(0)βˆ’(4)(βˆ’3sin⁑t),β€…β€Š(4)(βˆ’3cos⁑t)βˆ’(βˆ’3sin⁑t)(0),β€…β€Š(βˆ’3sin⁑t)(βˆ’3sin⁑t)βˆ’(3cos⁑t)(βˆ’3cos⁑t)⟩\vec{v} \times \vec{a} = \langle (3\cos t)(0) - (4)(-3\sin t), \; (4)(-3\cos t) - (-3\sin t)(0), \; (-3\sin t)(-3\sin t) - (3\cos t)(-3\cos t) \ranglevΓ—a=⟨(3cost)(0)βˆ’(4)(βˆ’3sint),(4)(βˆ’3cost)βˆ’(βˆ’3sint)(0),(βˆ’3sint)(βˆ’3sint)βˆ’(3cost)(βˆ’3cost)⟩
    vβƒ—Γ—aβƒ—=⟨12sin⁑t,β€…β€Šβˆ’12cos⁑t,β€…β€Š9(sin⁑2t+cos⁑2t)⟩=⟨12sin⁑t,β€…β€Šβˆ’12cos⁑t,β€…β€Š9⟩\vec{v} \times \vec{a} = \langle 12\sin t, \; -12\cos t, \; 9(\sin^2 t + \cos^2 t) \rangle = \langle 12\sin t, \; -12\cos t, \; 9 \ranglevΓ—a=⟨12sint,βˆ’12cost,9(sin2t+cos2t)⟩=⟨12sint,βˆ’12cost,9⟩

    Compute magnitude:

    βˆ₯vβƒ—Γ—aβƒ—βˆ₯=(12sin⁑t)2+(βˆ’12cos⁑t)2+92=144(sin⁑2t+cos⁑2t)+81=144+81=225=15\|\vec{v} \times \vec{a}\| = \sqrt{(12\sin t)^2 + (-12\cos t)^2 + 9^2} = \sqrt{144(\sin^2 t + \cos^2 t) + 81} = \sqrt{144 + 81} = \sqrt{225} = 15βˆ₯vΓ—aβˆ₯=(12sint)2+(βˆ’12cost)2+92​=144(sin2t+cos2t)+81​=144+81​=225​=15

    Evaluate curvature:

    ΞΊ=1553=15125=325=0.12Β unitsβˆ’1\kappa = \frac{15}{5^3} = \frac{15}{125} = \frac{3}{25} = 0.12\text{ units}^{-1}ΞΊ=5315​=12515​=253​=0.12Β unitsβˆ’1
    (Radius of curvature is ρ=1ΞΊ=253β‰ˆ8.33Β units\rho = \frac{1}{\kappa} = \frac{25}{3} \approx 8.33\text{ units}ρ=ΞΊ1​=325β€‹β‰ˆ8.33Β units.)

  4. Compute Tangential and Normal Acceleration Components: State the Tangential Acceleration Formula:

    aT=vβƒ—β‹…aβƒ—βˆ₯vβƒ—βˆ₯=(βˆ’3sin⁑t)(βˆ’3cos⁑t)+(3cos⁑t)(βˆ’3sin⁑t)+(4)(0)5=9sin⁑tcos⁑tβˆ’9sin⁑tcos⁑t5=0a_T = \frac{\vec{v} \cdot \vec{a}}{\|\vec{v}\|} = \frac{(-3\sin t)(-3\cos t) + (3\cos t)(-3\sin t) + (4)(0)}{5} = \frac{9\sin t\cos t - 9\sin t\cos t}{5} = 0aT​=βˆ₯vβˆ₯vβ‹…a​=5(βˆ’3sint)(βˆ’3cost)+(3cost)(βˆ’3sint)+(4)(0)​=59sintcostβˆ’9sintcost​=0
    (Because speed is constant, rate of speed change is identically zero).

    State the Normal Acceleration Formula:

    aN=βˆ₯vβƒ—Γ—aβƒ—βˆ₯βˆ₯vβƒ—βˆ₯=155=3Β units/s2a_N = \frac{\|\vec{v} \times \vec{a}\|}{\|\vec{v}\|} = \frac{15}{5} = 3\text{ units/s}^2aN​=βˆ₯vβˆ₯βˆ₯vΓ—aβˆ₯​=515​=3Β units/s2
    (Notice that aN=ΞΊβˆ₯vβƒ—βˆ₯2=(325)(25)=3a_N = \kappa \|\vec{v}\|^2 = \left(\frac{3}{25}\right)(25) = 3aN​=ΞΊβˆ₯vβˆ₯2=(253​)(25)=3, matching exactly).

Practice Problem 7: Concept & Reading Check

Open this Skill Block on the Memex to locate the information needed to answer the following:

  • (a) Explain why a particle traveling at a strictly constant scalar speed (v(t)=cv(t) = cv(t)=c) has aT=0a_T = 0aT​=0, but can still experience a non-zero acceleration vector aβƒ—(t)\vec{a}(t)a(t).
  • (b) Deconstruct the denominator of the cross-product curvature formula ΞΊ=βˆ₯vβƒ—Γ—aβƒ—βˆ₯βˆ₯vβƒ—βˆ₯3\kappa = \frac{\|\vec{v} \times \vec{a}\|}{\|\vec{v}\|^3}ΞΊ=βˆ₯vβˆ₯3βˆ₯vΓ—aβˆ₯​: why is speed cubed rather than squared?
  • (c) In Roller Coaster Loop Structural Dynamics (Entertainment & Mechanical Engineering), how does normal centripetal acceleration aNa_NaN​ relate to passenger safety G-force limits?
Solution Key:
  • (a) Tangential vs Normal Acceleration: Kinematic acceleration aβƒ—(t)=aTT^+aNN^\vec{a}(t) = a_T \hat{T} + a_N \hat{N}a(t)=aT​T^+aN​N^ decomposes into two independent physical mechanisms. The tangential component aT=ddtβˆ₯vβƒ—βˆ₯a_T = \frac{d}{dt}\|\vec{v}\|aT​=dtd​βˆ₯vβˆ₯ quantifies scalar throttle or braking. If speed is constant, aT=0a_T = 0aT​=0. However, whenever a curve changes directional heading in space, the unit tangent vector rotates (dT^/dtβ‰ 0βƒ—d\hat{T}/dt \ne \vec{0}dT^/dtξ€ =0). This directional rate of change generates a strictly perpendicular centripetal acceleration vector aNN^a_N \hat{N}aN​N^, meaning aβƒ—(t)=aNN^β‰ 0βƒ—\vec{a}(t) = a_N \hat{N} \ne \vec{0}a(t)=aN​N^ξ€ =0.
  • (b) Curvature Denominator Derivation: By definition, curvature is turning per unit distance: ΞΊ=βˆ₯T^β€²(t)βˆ₯βˆ₯rβƒ—β€²(t)βˆ₯=aNβˆ₯vβƒ—βˆ₯2\kappa = \frac{\|\hat{T}'(t)\|}{\|\vec{r}'(t)\|} = \frac{a_N}{\|\vec{v}\|^2}ΞΊ=βˆ₯rβ€²(t)βˆ₯βˆ₯T^β€²(t)βˆ₯​=βˆ₯vβˆ₯2aN​​. Because the normal acceleration formula evaluates to aN=βˆ₯vβƒ—Γ—aβƒ—βˆ₯βˆ₯vβƒ—βˆ₯a_N = \frac{\|\vec{v} \times \vec{a}\|}{\|\vec{v}\|}aN​=βˆ₯vβˆ₯βˆ₯vΓ—aβˆ₯​, substituting aNa_NaN​ into the curvature expression produces:
    ΞΊ=βˆ₯vβƒ—Γ—aβƒ—βˆ₯βˆ₯vβƒ—βˆ₯βˆ₯vβƒ—βˆ₯2=βˆ₯vβƒ—Γ—aβƒ—βˆ₯βˆ₯vβƒ—βˆ₯3\kappa = \frac{\frac{\|\vec{v} \times \vec{a}\|}{\|\vec{v}\|}}{\|\vec{v}\|^2} = \frac{\|\vec{v} \times \vec{a}\|}{\|\vec{v}\|^3}ΞΊ=βˆ₯vβˆ₯2βˆ₯vβˆ₯βˆ₯vΓ—aβˆ₯​​=βˆ₯vβˆ₯3βˆ₯vΓ—aβˆ₯​
  • (c) Biomechanical G-Force Limits: In amusement park and aerospace engineering, passenger bodies experience apparent weight and inertial load proportional to net acceleration via Newton's Second Law (Fβƒ—seatβˆ’mgβƒ—=maβƒ—\vec{F}_{\text{seat}} - m\vec{g} = m\vec{a}Fseatβ€‹βˆ’mg​=ma). The normal component aN=ΞΊv2=v2ρa_N = \kappa v^2 = \frac{v^2}{\rho}aN​=ΞΊv2=ρv2​ produces centripetal load. Dividing aNa_NaN​ by standard gravitational acceleration (g=9.81Β m/s2g = 9.81\text{ m/s}^2g=9.81Β m/s2) gives the added G-force loading. Keeping aNa_NaN​ within bounded limits (≀1.0Β g\le 1.0\text{ g}≀1.0Β g lateral, ≀4.5Β g\le 4.5\text{ g}≀4.5Β g vertical) prevents loss of consciousness (blackout) and severe neck strain.
Show your steps and calculations here.

Practice Problem 8

A precision automated machining cutter travels along the 3D space curve:

rβƒ—(t)=⟨2t,β€…β€Št2,β€…β€Š13t3⟩forΒ tβ‰₯0\vec{r}(t) = \langle 2t, \; t^2, \; \frac{1}{3}t^3 \rangle \quad \text{for } t \ge 0r(t)=⟨2t,t2,31​t3⟩forΒ tβ‰₯0

  1. Find the velocity vβƒ—(t)\vec{v}(t)v(t), acceleration aβƒ—(t)\vec{a}(t)a(t), and scalar speed βˆ₯vβƒ—(t)βˆ₯\|\vec{v}(t)\|βˆ₯v(t)βˆ₯.
  2. Compute the exact arc length sss traversed by the tool from t=0t = 0t=0 to t=3t = 3t=3.
  3. At the waypoint t=1t = 1t=1, compute the tangential acceleration aT(1)a_T(1)aT​(1), normal acceleration aN(1)a_N(1)aN​(1), and the curvature ΞΊ(1)\kappa(1)ΞΊ(1).
Solution Key:
  1. Differentiate and Compute Scalar Speed: State the Vector Derivative Formulas:

    vβƒ—(t)=rβƒ—β€²(t)=⟨2,β€…β€Š2t,β€…β€Št2⟩\vec{v}(t) = \vec{r}'(t) = \langle 2, \; 2t, \; t^2 \ranglev(t)=rβ€²(t)=⟨2,2t,t2⟩
    aβƒ—(t)=rβƒ—β€²β€²(t)=⟨0,β€…β€Š2,β€…β€Š2t⟩\vec{a}(t) = \vec{r}''(t) = \langle 0, \; 2, \; 2t \ranglea(t)=rβ€²β€²(t)=⟨0,2,2t⟩
    (Defined in Derivatives of Vector-Valued Functions.)

    State the Scalar Speed Formula:

    βˆ₯vβƒ—(t)βˆ₯=22+(2t)2+(t2)2=4+4t2+t4\|\vec{v}(t)\| = \sqrt{2^2 + (2t)^2 + (t^2)^2} = \sqrt{4 + 4t^2 + t^4}βˆ₯v(t)βˆ₯=22+(2t)2+(t2)2​=4+4t2+t4​
    Factor the perfect square trinomial under the radical:
    βˆ₯vβƒ—(t)βˆ₯=(t2+2)2=t2+2\|\vec{v}(t)\| = \sqrt{(t^2 + 2)^2} = t^2 + 2βˆ₯v(t)βˆ₯=(t2+2)2​=t2+2

  2. Compute Arc Length (0≀t≀30 \le t \le 30≀t≀3): State the Definite Arc Length Formula:

    s=∫abβˆ₯vβƒ—(t)βˆ₯ dts = \int_{a}^{b} \|\vec{v}(t)\|\,dts=∫ab​βˆ₯v(t)βˆ₯dt
    (Defined in Arc Length of a Space Curve.)

    s=∫03(t2+2) dt=[13t3+2t]03=(13(27)+2(3))βˆ’0=9+6=15Β unitss = \int_{0}^{3} (t^2 + 2)\,dt = \left[ \frac{1}{3}t^3 + 2t \right]_{0}^{3} = \left( \frac{1}{3}(27) + 2(3) \right) - 0 = 9 + 6 = 15\text{ units}s=∫03​(t2+2)dt=[31​t3+2t]03​=(31​(27)+2(3))βˆ’0=9+6=15Β units

  3. Evaluate at t=1t = 1t=1:

    • Velocity at t=1t = 1t=1:
      vβƒ—(1)=⟨2,2,1βŸ©β€…β€ŠβŸΉβ€…β€Šβˆ₯vβƒ—(1)βˆ₯=12+2=3\vec{v}(1) = \langle 2, 2, 1 \rangle \implies \|\vec{v}(1)\| = 1^2 + 2 = 3v(1)=⟨2,2,1⟩⟹βˆ₯v(1)βˆ₯=12+2=3
    • Acceleration at t=1t = 1t=1:
      aβƒ—(1)=⟨0,2,2βŸ©β€…β€ŠβŸΉβ€…β€Šβˆ₯aβƒ—(1)βˆ₯=02+22+22=8=22\vec{a}(1) = \langle 0, 2, 2 \rangle \implies \|\vec{a}(1)\| = \sqrt{0^2 + 2^2 + 2^2} = \sqrt{8} = 2\sqrt{2}a(1)=⟨0,2,2⟩⟹βˆ₯a(1)βˆ₯=02+22+22​=8​=22​
    • Dot product vβƒ—(1)β‹…aβƒ—(1)\vec{v}(1) \cdot \vec{a}(1)v(1)β‹…a(1):
      v⃗(1)⋅a⃗(1)=(2)(0)+(2)(2)+(1)(2)=0+4+2=6\vec{v}(1) \cdot \vec{a}(1) = (2)(0) + (2)(2) + (1)(2) = 0 + 4 + 2 = 6v(1)⋅a(1)=(2)(0)+(2)(2)+(1)(2)=0+4+2=6

    State the Tangential Acceleration Formula:

    aT(1)=vβƒ—(1)β‹…aβƒ—(1)βˆ₯vβƒ—(1)βˆ₯=63=2Β units/s2a_T(1) = \frac{\vec{v}(1) \cdot \vec{a}(1)}{\|\vec{v}(1)\|} = \frac{6}{3} = 2\text{ units/s}^2aT​(1)=βˆ₯v(1)βˆ₯v(1)β‹…a(1)​=36​=2Β units/s2
    (Notice that differentiating speed directly: aT=ddt[t2+2]=2ta_T = \frac{d}{dt}[t^2 + 2] = 2taT​=dtd​[t2+2]=2t, which at t=1t=1t=1 gives 222).

    State the Normal Acceleration Pythagorean Formula:

    aN(1)=βˆ₯aβƒ—(1)βˆ₯2βˆ’aT(1)2=(22)2βˆ’(2)2=8βˆ’4=4=2Β units/s2a_N(1) = \sqrt{\|\vec{a}(1)\|^2 - a_T(1)^2} = \sqrt{(2\sqrt{2})^2 - (2)^2} = \sqrt{8 - 4} = \sqrt{4} = 2\text{ units/s}^2aN​(1)=βˆ₯a(1)βˆ₯2βˆ’aT​(1)2​=(22​)2βˆ’(2)2​=8βˆ’4​=4​=2Β units/s2

    State the Curvature Formula:

    ΞΊ(1)=aN(1)βˆ₯vβƒ—(1)βˆ₯2=232=29Β unitsβˆ’1\kappa(1) = \frac{a_N(1)}{\|\vec{v}(1)\|^2} = \frac{2}{3^2} = \frac{2}{9}\text{ units}^{-1}ΞΊ(1)=βˆ₯v(1)βˆ₯2aN​(1)​=322​=92​ unitsβˆ’1
    (Radius of curvature at t=1t = 1t=1 is ρ=1ΞΊ=92=4.5Β units\rho = \frac{1}{\kappa} = \frac{9}{2} = 4.5\text{ units}ρ=ΞΊ1​=29​=4.5Β units).

Show your steps and calculations here.

Practice Problem 9

A weather tracking drone ascends along the circular helix space curve:

rβƒ—(t)=⟨4cos⁑t,β€…β€Š4sin⁑t,β€…β€Š3t⟩forΒ tβ‰₯0\vec{r}(t) = \langle 4\cos t, \; 4\sin t, \; 3t \rangle \quad \text{for } t \ge 0r(t)=⟨4cost,4sint,3t⟩forΒ tβ‰₯0

  1. Determine the velocity vector vβƒ—(t)\vec{v}(t)v(t), acceleration vector aβƒ—(t)\vec{a}(t)a(t), and scalar speed βˆ₯vβƒ—(t)βˆ₯\|\vec{v}(t)\|βˆ₯v(t)βˆ₯.
  2. Compute the unit tangent vector T^(t)\hat{T}(t)T^(t) and principal unit normal vector N^(t)=T^β€²(t)βˆ₯T^β€²(t)βˆ₯\hat{N}(t) = \frac{\hat{T}'(t)}{\|\hat{T}'(t)\|}N^(t)=βˆ₯T^β€²(t)βˆ₯T^β€²(t)​.
  3. Calculate the curvature ΞΊ(t)\kappa(t)ΞΊ(t), the radius of the osculating circle ρ\rhoρ, and decompose the acceleration into tangential and normal components (aTa_TaT​ and aNa_NaN​).
Solution Key:
  1. Differentiate and Compute Scalar Speed: State the Vector Derivative Formulas:

    vβƒ—(t)=rβƒ—β€²(t)=βŸ¨βˆ’4sin⁑t,β€…β€Š4cos⁑t,β€…β€Š3⟩\vec{v}(t) = \vec{r}'(t) = \langle -4\sin t, \; 4\cos t, \; 3 \ranglev(t)=rβ€²(t)=βŸ¨βˆ’4sint,4cost,3⟩
    aβƒ—(t)=rβƒ—β€²β€²(t)=βŸ¨βˆ’4cos⁑t,β€…β€Šβˆ’4sin⁑t,β€…β€Š0⟩\vec{a}(t) = \vec{r}''(t) = \langle -4\cos t, \; -4\sin t, \; 0 \ranglea(t)=rβ€²β€²(t)=βŸ¨βˆ’4cost,βˆ’4sint,0⟩

    State the Scalar Speed Formula:

    βˆ₯vβƒ—(t)βˆ₯=(βˆ’4sin⁑t)2+(4cos⁑t)2+32=16(sin⁑2t+cos⁑2t)+9=16+9=25=5Β units/s\|\vec{v}(t)\| = \sqrt{(-4\sin t)^2 + (4\cos t)^2 + 3^2} = \sqrt{16(\sin^2 t + \cos^2 t) + 9} = \sqrt{16 + 9} = \sqrt{25} = 5\text{ units/s}βˆ₯v(t)βˆ₯=(βˆ’4sint)2+(4cost)2+32​=16(sin2t+cos2t)+9​=16+9​=25​=5Β units/s

  2. Compute Unit Tangent Vector T^(t)\hat{T}(t)T^(t) and Principal Unit Normal Vector N^(t)\hat{N}(t)N^(t): State the Unit Tangent Vector Formula:

    T^(t)=vβƒ—(t)βˆ₯vβƒ—(t)βˆ₯=15βŸ¨βˆ’4sin⁑t,β€…β€Š4cos⁑t,β€…β€Š3⟩=βŸ¨βˆ’45sin⁑t,β€…β€Š45cos⁑t,β€…β€Š35⟩\hat{T}(t) = \frac{\vec{v}(t)}{\|\vec{v}(t)\|} = \frac{1}{5}\langle -4\sin t, \; 4\cos t, \; 3 \rangle = \left\langle -\frac{4}{5}\sin t, \; \frac{4}{5}\cos t, \; \frac{3}{5} \right\rangleT^(t)=βˆ₯v(t)βˆ₯v(t)​=51β€‹βŸ¨βˆ’4sint,4cost,3⟩=βŸ¨βˆ’54​sint,54​cost,53β€‹βŸ©

    Differentiate T^(t)\hat{T}(t)T^(t) with respect to ttt:

    T^β€²(t)=βŸ¨βˆ’45cos⁑t,β€…β€Šβˆ’45sin⁑t,β€…β€Š0⟩\hat{T}'(t) = \left\langle -\frac{4}{5}\cos t, \; -\frac{4}{5}\sin t, \; 0 \right\rangleT^β€²(t)=βŸ¨βˆ’54​cost,βˆ’54​sint,0⟩
    Compute its magnitude:
    βˆ₯T^β€²(t)βˆ₯=(βˆ’45cos⁑t)2+(βˆ’45sin⁑t)2+02=1625(cos⁑2t+sin⁑2t)=45\|\hat{T}'(t)\| = \sqrt{\left(-\frac{4}{5}\cos t\right)^2 + \left(-\frac{4}{5}\sin t\right)^2 + 0^2} = \sqrt{\frac{16}{25}(\cos^2 t + \sin^2 t)} = \frac{4}{5}βˆ₯T^β€²(t)βˆ₯=(βˆ’54​cost)2+(βˆ’54​sint)2+02​=2516​(cos2t+sin2t)​=54​

    State the Principal Unit Normal Formula:

    N^(t)=T^β€²(t)βˆ₯T^β€²(t)βˆ₯=54βŸ¨βˆ’45cos⁑t,β€…β€Šβˆ’45sin⁑t,β€…β€Š0⟩=βŸ¨βˆ’cos⁑t,β€…β€Šβˆ’sin⁑t,β€…β€Š0⟩\hat{N}(t) = \frac{\hat{T}'(t)}{\|\hat{T}'(t)\|} = \frac{5}{4}\left\langle -\frac{4}{5}\cos t, \; -\frac{4}{5}\sin t, \; 0 \right\rangle = \langle -\cos t, \; -\sin t, \; 0 \rangleN^(t)=βˆ₯T^β€²(t)βˆ₯T^β€²(t)​=45β€‹βŸ¨βˆ’54​cost,βˆ’54​sint,0⟩=βŸ¨βˆ’cost,βˆ’sint,0⟩
    (Defined in Principal Unit Normal Vector.)

  3. Compute Curvature, Osculating Radius, and Acceleration Components: State the Curvature Formula:

    ΞΊ=βˆ₯T^β€²(t)βˆ₯βˆ₯rβƒ—β€²(t)βˆ₯=4/55=425=0.16Β unitsβˆ’1\kappa = \frac{\|\hat{T}'(t)\|}{\|\vec{r}'(t)\|} = \frac{4/5}{5} = \frac{4}{25} = 0.16\text{ units}^{-1}ΞΊ=βˆ₯rβ€²(t)βˆ₯βˆ₯T^β€²(t)βˆ₯​=54/5​=254​=0.16Β unitsβˆ’1

    State the Radius of Curvature Formula:

    ρ=1ΞΊ=254=6.25Β units\rho = \frac{1}{\kappa} = \frac{25}{4} = 6.25\text{ units}ρ=ΞΊ1​=425​=6.25Β units

    State the Tangential Acceleration Formula:

    aT=ddtβˆ₯vβƒ—(t)βˆ₯=ddt[5]=0Β units/s2a_T = \frac{d}{dt}\|\vec{v}(t)\| = \frac{d}{dt}[5] = 0\text{ units/s}^2aT​=dtd​βˆ₯v(t)βˆ₯=dtd​[5]=0Β units/s2

    State the Normal Acceleration Formula:

    aN=ΞΊβˆ₯vβƒ—βˆ₯2=(425)(52)=(425)(25)=4Β units/s2a_N = \kappa \|\vec{v}\|^2 = \left(\frac{4}{25}\right)(5^2) = \left(\frac{4}{25}\right)(25) = 4\text{ units/s}^2aN​=ΞΊβˆ₯vβˆ₯2=(254​)(52)=(254​)(25)=4Β units/s2
    (Notice that aβƒ—(t)=aTT^+aNN^=0T^+4βŸ¨βˆ’cos⁑t,βˆ’sin⁑t,0⟩=βŸ¨βˆ’4cos⁑t,βˆ’4sin⁑t,0⟩\vec{a}(t) = a_T \hat{T} + a_N \hat{N} = 0\hat{T} + 4\langle -\cos t, -\sin t, 0 \rangle = \langle -4\cos t, -4\sin t, 0 \ranglea(t)=aT​T^+aN​N^=0T^+4βŸ¨βˆ’cost,βˆ’sint,0⟩=βŸ¨βˆ’4cost,βˆ’4sint,0⟩, matching rβƒ—β€²β€²(t)\vec{r}''(t)rβ€²β€²(t) exactly).


Show your steps and calculations here.

Regroup 3

  • Algebraic Speed Check: Always check if the quadratic under the radical in βˆ₯vβƒ—(t)βˆ₯\|\vec{v}(t)\|βˆ₯v(t)βˆ₯ factors as a perfect square (at2+b)2(at^2 + b)^2(at2+b)2. This is a classic exam technique that avoids intractable radical integrals.
  • Normal Acceleration Positivity: aNa_NaN​ is a geometric magnitude (aN=ΞΊv2β‰₯0a_N = \kappa v^2 \ge 0aN​=ΞΊv2β‰₯0). It can NEVER be negative! If your calculation yields a negative value, recheck your dot product and magnitude substitutions.

Synthesis Wrap-up

  • Exam Formula Strategy: State every governing symbolic equation before substituting numerical values to secure partial credit and prevent arithmetic slips.
  • Test Review Center Recovery Protocol: Remember that logging 4 active hours in the Test Review Center allows you to convert one pure 0% homework score into 100% (up to 2 assignments), restoring your retroactive midterm grade replacement eligibility.
  • Exam Readiness Checklist:
    1. Can you set up and calculate projuβƒ—vβƒ—\text{proj}_{\vec{u}}\vec{v}proju​v and uβƒ—Γ—vβƒ—\vec{u} \times \vec{v}uΓ—v without mixing up formulas?
    2. Can you write symmetric line equations and compute point-to-line perpendicular distances?
    3. Can you find vβƒ—(t),aβƒ—(t)\vec{v}(t), \vec{a}(t)v(t),a(t), arc length sss, curvature ΞΊ\kappaΞΊ, and tangential/normal acceleration components aT,aNa_T, a_NaT​,aN​?