Core Definition
If r ⃗ ( t ) = ⟨ f ( t ) , g ( t ) , h ( t ) ⟩ = f ( t ) i ^ + g ( t ) j ^ + h ( t ) k ^ \vec{r}(t) = \langle f(t), g(t), h(t) \rangle = f(t)\hat{i} + g(t)\hat{j} + h(t)\hat{k} r ( t ) = ⟨ f ( t ) , g ( t ) , h ( t )⟩ = f ( t ) i ^ + g ( t ) j ^ + h ( t ) k ^ is a continuous vector-valued function on an interval [ a , b ] [a, b] [ a , b ] , its integral is evaluated component-wise:
Indefinite Integral:
∫ r ⃗ ( t ) d t = ( ∫ f ( t ) d t ) i ^ + ( ∫ g ( t ) d t ) j ^ + ( ∫ h ( t ) d t ) k ^ = R ⃗ ( t ) + C ⃗ \int \vec{r}(t) \, dt = \left( \int f(t) \, dt \right)\hat{i} + \left( \int g(t) \, dt \right)\hat{j} + \left( \int h(t) \, dt \right)\hat{k} = \vec{R}(t) + \vec{C} ∫ r ( t ) d t = ( ∫ f ( t ) d t ) i ^ + ( ∫ g ( t ) d t ) j ^ + ( ∫ h ( t ) d t ) k ^ = R ( t ) + C
where R ⃗ ( t ) = ⟨ F ( t ) , G ( t ) , H ( t ) ⟩ \vec{R}(t) = \langle F(t), G(t), H(t) \rangle R ( t ) = ⟨ F ( t ) , G ( t ) , H ( t )⟩ is an antiderivative vector and C ⃗ = ⟨ C 1 , C 2 , C 3 ⟩ \vec{C} = \langle C_1, C_2, C_3 \rangle C = ⟨ C 1 , C 2 , C 3 ⟩ is an arbitrary constant vector of integration .
Definite Integral (Fundamental Theorem of Calculus in R 3 \mathbb{R}^3 R 3 ):
∫ a b r ⃗ ( t ) d t = ⟨ ∫ a b f ( t ) d t , ∫ a b g ( t ) d t , ∫ a b h ( t ) d t ⟩ = R ⃗ ( b ) − R ⃗ ( a ) \int_{a}^{b} \vec{r}(t) \, dt = \left\langle \int_{a}^{b} f(t) \, dt, \int_{a}^{b} g(t) \, dt, \int_{a}^{b} h(t) \, dt \right\rangle = \vec{R}(b) - \vec{R}(a) ∫ a b r ( t ) d t = ⟨ ∫ a b f ( t ) d t , ∫ a b g ( t ) d t , ∫ a b h ( t ) d t ⟩ = R ( b ) − R ( a )
Concept Explanation
Indefinite Integrals & The Constant Vector C ⃗ \vec{C} C
When integrating scalar functions, a single integration constant + C + C + C is produced. Because a 3D vector-valued function consists of three independent component integrations, each component produces its own independent constant (C 1 , C 2 , C 3 C_1, C_2, C_3 C 1 , C 2 , C 3 ):
∫ r ⃗ ( t ) d t = ⟨ F ( t ) + C 1 , G ( t ) + C 2 , H ( t ) + C 3 ⟩ = ⟨ F ( t ) , G ( t ) , H ( t ) ⟩ + ⟨ C 1 , C 2 , C 3 ⟩ = R ⃗ ( t ) + C ⃗ \int \vec{r}(t) \, dt = \langle F(t) + C_1, G(t) + C_2, H(t) + C_3 \rangle = \langle F(t), G(t), H(t) \rangle + \langle C_1, C_2, C_3 \rangle = \vec{R}(t) + \vec{C} ∫ r ( t ) d t = ⟨ F ( t ) + C 1 , G ( t ) + C 2 , H ( t ) + C 3 ⟩ = ⟨ F ( t ) , G ( t ) , H ( t )⟩ + ⟨ C 1 , C 2 , C 3 ⟩ = R ( t ) + C
Never Leave
C ⃗ \vec{C} C as a Scalar
In vector calculus, the constant of integration C ⃗ \vec{C} C must be a vector ⟨ C 1 , C 2 , C 3 ⟩ \langle C_1, C_2, C_3 \rangle ⟨ C 1 , C 2 , C 3 ⟩ . Writing + C +\, C + C (a scalar added to a vector) is algebraically invalid.
Physical Kinematics & Initial Value Problems (IVPs)
Integrating vector-valued functions allows engineers to recover position and velocity profiles from acceleration data:
From Acceleration to Velocity:
v ⃗ ( t ) = ∫ a ⃗ ( t ) d t + C ⃗ 1 ⟹ Given v ⃗ ( 0 ) = v ⃗ 0 ⟹ C ⃗ 1 = v ⃗ 0 − V ⃗ ( 0 ) \vec{v}(t) = \int \vec{a}(t) \, dt + \vec{C}_1 \implies \text{Given } \vec{v}(0) = \vec{v}_0 \implies \vec{C}_1 = \vec{v}_0 - \vec{V}(0) v ( t ) = ∫ a ( t ) d t + C 1 ⟹ Given v ( 0 ) = v 0 ⟹ C 1 = v 0 − V ( 0 )
From Velocity to Position:
r ⃗ ( t ) = ∫ v ⃗ ( t ) d t + C ⃗ 2 ⟹ Given r ⃗ ( 0 ) = r ⃗ 0 ⟹ C ⃗ 2 = r ⃗ 0 − R ⃗ ( 0 ) \vec{r}(t) = \int \vec{v}(t) \, dt + \vec{C}_2 \implies \text{Given } \vec{r}(0) = \vec{r}_0 \implies \vec{C}_2 = \vec{r}_0 - \vec{R}(0) r ( t ) = ∫ v ( t ) d t + C 2 ⟹ Given r ( 0 ) = r 0 ⟹ C 2 = r 0 − R ( 0 )
Definite Integrals: Net Displacement
Evaluating the definite integral of velocity v ⃗ ( t ) \vec{v}(t) v ( t ) over a time interval a ≤ t ≤ b a \le t \le b a ≤ t ≤ b yields the net displacement vector Δ r ⃗ \Delta \vec{r} Δ r :
Δ r ⃗ = r ⃗ ( b ) − r ⃗ ( a ) = ∫ a b v ⃗ ( t ) d t \Delta \vec{r} = \vec{r}(b) - \vec{r}(a) = \int_{a}^{b} \vec{v}(t) \, dt Δ r = r ( b ) − r ( a ) = ∫ a b v ( t ) d t
The displacement vector Δ r ⃗ \Delta \vec{r} Δ r represents the straight-line directed vector connecting the starting point r ⃗ ( a ) \vec{r}(a) r ( a ) directly to the ending point r ⃗ ( b ) \vec{r}(b) r ( b ) in R 3 \mathbb{R}^3 R 3 .
Engineering Applications
Inertial Navigation Systems (Dead Reckoning): Reconstructing 3D aircraft and submarine positions from onboard 3-axis accelerometer time-series data.
Structural Vibration & Shock Analysis: Integrating measured dynamic acceleration logs to evaluate transient structural deflection envelopes in bridges and skyscrapers.
Electric Vehicle Dynamics: Computing motor speed and vehicle displacement from current-regulated torque and acceleration profiles.
Example Problems
Example 1: Indefinite Vector Integration
Evaluate the indefinite integral:
∫ ⟨ 5 cos ( 7 t ) , 3 cos ( 4 t ) , − 9 t ⟩ d t \int \left\langle 5\cos(7t), 3\cos(4t), \frac{-9}{t} \right\rangle dt ∫ ⟨ 5 cos ( 7 t ) , 3 cos ( 4 t ) , t − 9 ⟩ d t
Solution
Integrate Component 1 (x x x -component):
∫ 5 cos ( 7 t ) d t = 5 7 sin ( 7 t ) + C 1 \int 5\cos(7t) \, dt = \frac{5}{7}\sin(7t) + C_1 ∫ 5 cos ( 7 t ) d t = 7 5 sin ( 7 t ) + C 1
Integrate Component 2 (y y y -component):
∫ 3 cos ( 4 t ) d t = 3 4 sin ( 4 t ) + C 2 \int 3\cos(4t) \, dt = \frac{3}{4}\sin(4t) + C_2 ∫ 3 cos ( 4 t ) d t = 4 3 sin ( 4 t ) + C 2
Integrate Component 3 (z z z -component):
∫ − 9 t d t = − 9 ln ∣ t ∣ + C 3 \int \frac{-9}{t} \, dt = -9\ln|t| + C_3 ∫ t − 9 d t = − 9 ln ∣ t ∣ + C 3
Combine into Vector Form with C ⃗ \vec{C} C :
∫ ⟨ 5 cos ( 7 t ) , 3 cos ( 4 t ) , − 9 t ⟩ d t = ⟨ 5 7 sin ( 7 t ) , 3 4 sin ( 4 t ) , − 9 ln ∣ t ∣ ⟩ + C ⃗ \int \left\langle 5\cos(7t), 3\cos(4t), \frac{-9}{t} \right\rangle dt = \left\langle \frac{5}{7}\sin(7t), \frac{3}{4}\sin(4t), -9\ln|t| \right\rangle + \vec{C} ∫ ⟨ 5 cos ( 7 t ) , 3 cos ( 4 t ) , t − 9 ⟩ d t = ⟨ 7 5 sin ( 7 t ) , 4 3 sin ( 4 t ) , − 9 ln ∣ t ∣ ⟩ + C
where C ⃗ = ⟨ C 1 , C 2 , C 3 ⟩ \vec{C} = \langle C_1, C_2, C_3 \rangle C = ⟨ C 1 , C 2 , C 3 ⟩ .
Example 2: Initial Value Problem (Recovering Position from Acceleration)
An autonomous rover has acceleration a ⃗ ( t ) = ⟨ 6 t , 12 t 2 , 4 ⟩ m/s 2 \vec{a}(t) = \langle 6t, 12t^2, 4 \rangle \text{ m/s}^2 a ( t ) = ⟨ 6 t , 12 t 2 , 4 ⟩ m/s 2 with initial velocity v ⃗ ( 0 ) = ⟨ 2 , − 1 , 5 ⟩ m/s \vec{v}(0) = \langle 2, -1, 5 \rangle \text{ m/s} v ( 0 ) = ⟨ 2 , − 1 , 5 ⟩ m/s and initial position r ⃗ ( 0 ) = ⟨ 0 , 10 , − 3 ⟩ m \vec{r}(0) = \langle 0, 10, -3 \rangle \text{ m} r ( 0 ) = ⟨ 0 , 10 , − 3 ⟩ m . Find its position function r ⃗ ( t ) \vec{r}(t) r ( t ) .
Solution
Integrate Acceleration to find Velocity v ⃗ ( t ) \vec{v}(t) v ( t ) :
v ⃗ ( t ) = ∫ ⟨ 6 t , 12 t 2 , 4 ⟩ d t = ⟨ 3 t 2 , 4 t 3 , 4 t ⟩ + C ⃗ 1 \vec{v}(t) = \int \langle 6t, 12t^2, 4 \rangle \, dt = \langle 3t^2, 4t^3, 4t \rangle + \vec{C}_1 v ( t ) = ∫ ⟨ 6 t , 12 t 2 , 4 ⟩ d t = ⟨ 3 t 2 , 4 t 3 , 4 t ⟩ + C 1
Apply initial condition v ⃗ ( 0 ) = ⟨ 2 , − 1 , 5 ⟩ \vec{v}(0) = \langle 2, -1, 5 \rangle v ( 0 ) = ⟨ 2 , − 1 , 5 ⟩ :
v ⃗ ( 0 ) = ⟨ 0 , 0 , 0 ⟩ + C ⃗ 1 = ⟨ 2 , − 1 , 5 ⟩ ⟹ C ⃗ 1 = ⟨ 2 , − 1 , 5 ⟩ \vec{v}(0) = \langle 0, 0, 0 \rangle + \vec{C}_1 = \langle 2, -1, 5 \rangle \implies \vec{C}_1 = \langle 2, -1, 5 \rangle v ( 0 ) = ⟨ 0 , 0 , 0 ⟩ + C 1 = ⟨ 2 , − 1 , 5 ⟩ ⟹ C 1 = ⟨ 2 , − 1 , 5 ⟩
v ⃗ ( t ) = ⟨ 3 t 2 + 2 , 4 t 3 − 1 , 4 t + 5 ⟩ \vec{v}(t) = \langle 3t^2 + 2, 4t^3 - 1, 4t + 5 \rangle v ( t ) = ⟨ 3 t 2 + 2 , 4 t 3 − 1 , 4 t + 5 ⟩
Integrate Velocity to find Position r ⃗ ( t ) \vec{r}(t) r ( t ) :
r ⃗ ( t ) = ∫ ⟨ 3 t 2 + 2 , 4 t 3 − 1 , 4 t + 5 ⟩ d t = ⟨ t 3 + 2 t , t 4 − t , 2 t 2 + 5 t ⟩ + C ⃗ 2 \vec{r}(t) = \int \langle 3t^2 + 2, 4t^3 - 1, 4t + 5 \rangle \, dt = \langle t^3 + 2t, t^4 - t, 2t^2 + 5t \rangle + \vec{C}_2 r ( t ) = ∫ ⟨ 3 t 2 + 2 , 4 t 3 − 1 , 4 t + 5 ⟩ d t = ⟨ t 3 + 2 t , t 4 − t , 2 t 2 + 5 t ⟩ + C 2
Apply initial condition r ⃗ ( 0 ) = ⟨ 0 , 10 , − 3 ⟩ \vec{r}(0) = \langle 0, 10, -3 \rangle r ( 0 ) = ⟨ 0 , 10 , − 3 ⟩ :
r ⃗ ( 0 ) = ⟨ 0 , 0 , 0 ⟩ + C ⃗ 2 = ⟨ 0 , 10 , − 3 ⟩ ⟹ C ⃗ 2 = ⟨ 0 , 10 , − 3 ⟩ \vec{r}(0) = \langle 0, 0, 0 \rangle + \vec{C}_2 = \langle 0, 10, -3 \rangle \implies \vec{C}_2 = \langle 0, 10, -3 \rangle r ( 0 ) = ⟨ 0 , 0 , 0 ⟩ + C 2 = ⟨ 0 , 10 , − 3 ⟩ ⟹ C 2 = ⟨ 0 , 10 , − 3 ⟩
r ⃗ ( t ) = ⟨ t 3 + 2 t , t 4 − t + 10 , 2 t 2 + 5 t − 3 ⟩ m \vec{r}(t) = \langle t^3 + 2t, t^4 - t + 10, 2t^2 + 5t - 3 \rangle \text{ m} r ( t ) = ⟨ t 3 + 2 t , t 4 − t + 10 , 2 t 2 + 5 t − 3 ⟩ m
Connections & References