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Motion in Space
Describe the velocity and acceleration vectors of a particle moving in space.
Motion Vectors in the Plane and in Space
Our starting point is using vector-valued functions to represent the position of an object as a function of time. All of the following material can be applied either to curves in the plane or to space curves. For example, when we look at the orbit of the planets, the curves defining these orbits all lie in a plane because they are elliptical. However, a particle traveling along a helix moves on a curve in three dimensions.
Since \(\text{r}(t)\) can be in either two or three dimensions, these vector-valued functions can have either two or three components. In two dimensions, we define \(\text{r}(t)=x(t)\ \text{i}+y(t)\ \text{j}\) and in three dimensions \(\text{r}(t)=x(t)\ \text{i}+y(t)\ \text{j}+z(t)\ \text{k}.\) Then the velocity, acceleration, and speed can be written as shown in the following table.
| Quantity | Two Dimensions | Three Dimensions |
| Position | \(\text{r}(t)=x(t)\ \text{i}+y(t)\ \text{j}\) | \(\text{r}(t)=x(t)\ \text{i}+y(t)\ \text{j}+z(t)\ \text{k}\) |
| Velocity | \(\text{v}(t)={x}^{'}(t)\ \text{i}+{y}^{'}(t)\ \text{j}\) | \(\text{v}(t)={x}^{'}(t)\ \text{i}+{y}^{'}(t)\ \text{j}+{z}^{'}(t)\ \text{k}\) |
| Acceleration | \(\text{a}(t)={x}^{″}(t)\ \text{i}+{y}^{″}(t)\ \text{j}\) | \(\text{a}(t)={x}^{″}(t)\ \text{i}+{y}^{″}(t)\ \text{j}+{z}^{″}(t)\ \text{k}\) |
| Speed | \(v(t)=\sqrt{{({x}^{'}(t))}^{2}+{({y}^{'}(t))}^{2}}\) | \(v(t)=\sqrt{{({x}^{'}(t))}^{2}+{({y}^{'}(t))}^{2}+{({z}^{'}(t))}^{2}}\) |
Condensed — the full section is in OpenStax Calculus Volume 3.
Components of the Acceleration Vector
We can combine some of the concepts discussed in Arc Length and Curvature with the acceleration vector to gain a deeper understanding of how this vector relates to motion in the plane and in space. Recall that the unit tangent vector T and the unit normal vector N form an osculating plane at any point P on the curve defined by a vector-valued function \(\text{r}(t).\) The following theorem shows that the acceleration vector \(\text{a}(t)\) lies in the osculating plane and can be written as a linear combination of the unit tangent and the unit normal vectors.
Condensed — the full section is in OpenStax Calculus Volume 3.
Projectile Motion
Now let’s look at an application of vector functions. In particular, let’s consider the effect of gravity on the motion of an object as it travels through the air, and how it determines the resulting trajectory of that object. In the following, we ignore the effect of air resistance. This situation, with an object moving with an initial velocity but with no forces acting on it other than gravity, is known as projectile motion. It describes the motion of objects from golf balls to baseballs, and from arrows to cannonballs.
First we need to choose a coordinate system. If we are standing at the origin of this coordinate system, then we choose the positive y-axis to be up, the negative y-axis to be down, and the positive x-axis to be forward (i.e., away from the thrower of the object). The effect of gravity is in a downward direction, so Newton’s second law tells us that the force on the object resulting from gravity is equal to the mass of the object times the acceleration resulting from to gravity, or \({F}_{g}=mg,\) where \({F}_{g}\) represents the force from gravity and g represents the acceleration resulting from gravity at Earth’s surface. The value of g in the English system of measurement is approximately 32 ft/sec2 and it is approximately 9.8 m/sec2 in the metric system. This is the only force acting on the object. Since gravity acts in a downward direction, we can write the force resulting from gravity in the form \({F}_{g}=\text{-}mg\ \text{j},\) as shown in the following figure.
Newton’s second law also tells us that \(F=m\ \text{a},\) where a represents the acceleration vector of the object. This force must be equal to the force of gravity at all times, so we therefore know that
\[\begin{array}{lll}F & = & {F}_{g} \\ m\ \text{a} & = & \text{-}mg\ \text{j} \\ \text{a} & = & \text{-}g\ \text{j}.\end{array}\]Now we use the fact that the acceleration vector is the first derivative of the velocity vector. Therefore, we can rewrite the last equation in the form
\[{v}^{'}(t)=\text{-}g\ \text{j}.\]By taking the antiderivative of each side of this equation we obtain
\[\begin{array}{ll}\text{v}(t) & =\int \text{-}g\ \text{j}dt \\ & =\text{-}gt\ \text{j}+{\text{C}}_{1}\end{array}\]Next we use the fact that velocity \(\text{v}(t)\) is the derivative of position \(\text{s}(t).\) This gives the equation
\[{s}^{'}(t)=\text{-}gt\ \text{j}+{\text{v}}_{0}.\]\[\begin{array}{ll}\text{s}(t) & =\int \text{-}gt\ \text{j}+{\text{v}}_{0}dt \\ & =-\frac{1}{2}g{t}^{2}\text{j}+{\text{v}}_{0}t+{\text{C}}_{2},\end{array}\]Condensed — the full section is in OpenStax Calculus Volume 3.
Kepler’s Laws
During the early 1600s, Johannes Kepler was able to use the amazingly accurate data from his mentor Tycho Brahe to formulate his three laws of planetary motion, now known as Kepler’s laws of planetary motion. These laws also apply to other objects in the solar system in orbit around the Sun, such as comets (e.g., Halley’s comet) and asteroids. Variations of these laws apply to satellites in orbit around Earth.
Kepler’s third law is especially useful when using appropriate units. In particular, 1 astronomical unit is defined to be the average distance from Earth to the Sun, and is now recognized to be 149,597,870,700 m or, approximately 93,000,000 mi. We therefore write 1 A.U. = 93,000,000 mi. Since the time it takes for Earth to orbit the Sun is 1 year, we use Earth years for units of time. Then, substituting 1 year for the period of Earth and 1 A.U. for the average distance to the Sun, Kepler’s third law can be written as
\[{T}_{p}^{2}={D}_{p}^{3}\]for any planet in the solar system, where \({T}_{P}\) is the period of that planet measured in Earth years and \({D}_{P}\) is the average distance from that planet to the Sun measured in astronomical units. Therefore, if we know the average distance from a planet to the Sun (in astronomical units), we can then calculate the length of its year (in Earth years), and vice versa.
Kepler’s laws were formulated based on observations from Brahe; however, they were not proved formally until Sir Isaac Newton was able to apply calculus. Furthermore, Newton was able to generalize Kepler’s third law to other orbital systems, such as a moon orbiting around a planet. Kepler’s original third law only applies to objects orbiting the Sun.
Condensed — the full section is in OpenStax Calculus Volume 3.
Key Concepts
- If \(\text{r}(t)\) represents the position of an object at time t, then \(\text{r}'(t)\) represents the velocity and \(\text{r″}(t)\) represents the acceleration of the object at time t. The magnitude of the velocity vector is speed.
- The acceleration vector always points toward the concave side of the curve defined by \(\text{r}(t).\) The tangential and normal components of acceleration \({a}_{\text{T}}\) and \({a}_{\text{N}}\) are the projections of the acceleration vector onto the unit tangent and unit normal vectors to the curve.
- Kepler’s three laws of planetary motion describe the motion of objects in orbit around the Sun. His third law can be modified to describe motion of objects in orbit around other celestial objects as well.
- Newton was able to use his law of universal gravitation in conjunction with his second law of motion and calculus to prove Kepler’s three laws.
Key Equations
| Velocity | \(\text{v}(t)={r}^{'}(t)\) |
| Acceleration | \(\text{a}(t)={v}^{'}(t)=\text{r″}(t)\) |
| Speed | \(v(t)=‖\text{v}(t)‖=‖{r}^{'}(t)‖=\frac{ds}{dt}\) |
| Tangential component of acceleration | \({a}_{\text{T}}=\text{a}\cdot \text{T}=\frac{\text{v}\cdot \text{a}}{‖\text{v}‖}\) |
| Normal component of acceleration | \({a}_{\text{N}}=\text{a}\cdot \text{N}=\frac{‖\text{v}\ \times \ \text{a}‖}{‖\text{v}‖}=\sqrt{{‖\text{a}‖}^{2}-{a\ }_{\text{T}}^{2}}\) |
Motion in Space
Given the following position functions, find the velocity, acceleration, and speed in terms of the parameter t.
Find the velocity, acceleration, and speed of a particle with the given position function.
Consider the motion of a point on the circumference of a rolling circle. As the circle rolls, it generates the cycloid \(\text{r}(t)=(\omega t-\text{sin}(\omega t))\ \text{i}+(1-\text{cos}(\omega t))\ \text{j},\) where \(\omega\) is the angular velocity of the circle:
A person on a hang glider is spiraling upward as a result of the rapidly rising air on a path having position vector \(\text{r}(t)=(3\ \text{cos}\ t)\text{i}+(3\ \text{sin}\ t)\text{j}+{t}^{2}\text{k}.\) The path is similar to that of a helix, although it is not a helix. The graph is shown here:
Find the following quantities:
Given that \(\text{r}(t)=〈{e}^{-5t}\text{sin}\ t,{e}^{-5t}\text{cos}\ t,4{e}^{-5t}〉\) is the position vector of a moving particle, find the following quantities:
A projectile is shot in the air from ground level with an initial velocity of 500 m/sec at an angle of 60° with the horizontal. The graph is shown here:
Condensed — the full section is in OpenStax Calculus Volume 3.
Practice (40)
Try each one on paper first. Reveal the answer to check; verified ones can be opened in the solver for every step.
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A particle moves in a parabolic path defined by the vector-valued function \(\text{r}(t)={t}^{2}\text{i}+\sqrt{5-{t}^{2}}\text{j},\) where t measures time in seconds.
- Find the velocity, acceleration, and speed as functions of time.
- Sketch the curve along with the velocity vector at time \(t=1.\)
Rivela la risposta
- We use , , and :
\[\begin{array}{lll}\text{v}(t) & = & {r}^{'}(t)=2t\ \text{i}-\frac{t}{\sqrt{5-{t}^{2}}}\text{j} \\ \text{a}(t) & = & {v}^{'}(t)=2\text{i}-5{(5-{t}^{2})}^{-\frac{3}{2}}\text{j} \\ v(t) & = & ‖{r}^{'}(t)‖ \\ & = & \sqrt{{(2t)}^{2}+{(-\frac{t}{\sqrt{5-{t}^{2}}})}^{2}} \\ & = & \sqrt{4{t}^{2}+\frac{{t}^{2}}{5-{t}^{2}}} \\ & = & \sqrt{\frac{21{t}^{2}-4{t}^{4}}{5-{t}^{2}}}.\end{array}\] - The graph of \(\text{r}(t)={t}^{2}\text{i}+\sqrt{5-{t}^{2}}\text{j}\) is a portion of a parabola (). The velocity vector at \(t=1\) is
\[\text{v}(1)={r}^{'}(1)=2(1)\ \text{i}-\frac{1}{\sqrt{5-{(1)}^{2}}}\text{j}=2\text{i}-\frac{1}{2}\text{j}\]
and the acceleration vector at \(t=1\) is
\[\text{a}(1)={v}^{'}(1)=2\text{i}-5{(5-{(1)}^{2})}^{\text{-}3\text{/}2}\text{j}=2\text{i}-\frac{5}{8}\text{j}.\]
Notice that the velocity vector is tangent to the path, as is always the case.
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A particle moves in a path defined by the vector-valued function \(\text{r}(t)=({t}^{2}-3t)\ \text{i}+(2t-4)\ \text{j}+(t+2)\text{k},\) where t measures time in seconds and where distance is measured in feet. Find the velocity, acceleration, and speed as functions of time.
Rivela la risposta
\(\begin{array}{l}\text{v}(t)={r}^{'}(t)=(2t-3)\ \text{i}+2\text{j}+\text{k} \\ \text{a}(t)={v}^{'}(t)=2\text{i} \\ v(t)=‖{r}^{'}(t)‖=\sqrt{{(2t-3)}^{2}+{2}^{2}+{1}^{2}}=\sqrt{4{t}^{2}-12t+14}\end{array}\)
The units for velocity and speed are feet per second, and the units for acceleration are feet per second squared.
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A particle moves in a path defined by the vector-valued function \(\text{r}(t)={t}^{2}\text{i}+(2t-3)\ \text{j}+(3{t}^{2}-3t)\ \text{k},\) where t measures time in seconds and distance is measured in feet.
- Find \({a}_{\text{T}}\) and \({a}_{\text{N}}\) as functions of t.
- Find \({a}_{\text{T}}\) and \({a}_{\text{N}}\) at time \(t=2.\)
Rivela la risposta
- Let’s start with :
\[\begin{array}{lll}\text{v}(t) & = & {r}^{'}(t)=2t\ \text{i}+2\text{j}+(6t-3)\ \text{k} \\ \text{a}(t) & = & {v}^{'}(t)=2\text{i}+6\text{k} \\ {a}_{\text{T}} & = & \frac{\text{v}\cdot \text{a}}{‖\text{v}‖} \\ & = & \frac{(2t\ \text{i}+2\text{j}+(6t-3)\ \text{k})\cdot (2\text{i}+6\text{k})}{‖2t\ \text{i}+2\text{j}+(6t-3)\ \text{k}‖} \\ & = & \frac{4t+6(6t-3)}{\sqrt{{(2t)}^{2}+{2}^{2}+{(6t-3)}^{2}}} \\ & = & \frac{40t-18}{\sqrt{40{t}^{2}-36t+13}}.\end{array}\]
Then we apply :
\[\begin{array}{ll}{a}_{\text{N}} & =\sqrt{{‖\text{a}‖}^{2}-{a\ \text{T}}^{2}} \\ & =\sqrt{{‖2\text{i}+6\text{k}‖}^{2}-{(\frac{40t-18}{\sqrt{40{t}^{2}-36t+13}})}^{2}} \\ & =\sqrt{4+36-\frac{{(40t-18)}^{2}}{40{t}^{2}-36t+13}} \\ & =\sqrt{\frac{40(40{t}^{2}-36t+13)-(1600{t}^{2}-1440t+324)}{40{t}^{2}-36t+13}} \\ & =\sqrt{\frac{196}{40{t}^{2}-36t+13}} \\ & =\frac{14}{\sqrt{40{t}^{2}-36t+13}}.\end{array}\] - We must evaluate each of the answers from part a. at \(t=2\text{:}\)
\[\begin{array}{lll}{a}_{\text{T}}(2) & = & \frac{40(2)-18}{\sqrt{40{(2)}^{2}-36(2)+13}} \\ & = & \frac{80-18}{\sqrt{160-72+13}}=\frac{62}{\sqrt{101}} \\ {a}_{\text{N}}(2) & = & \frac{14}{\sqrt{40{(2)}^{2}-36(2)+13}} \\ & = & \frac{14}{\sqrt{160-72+13}}=\frac{14}{\sqrt{101}}.\end{array}\]
The units of acceleration are feet per second squared, as are the units of the normal and tangential components of acceleration.
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An object moves in a path defined by the vector-valued function \(\text{r}(t)=4t\ \text{i}+{t}^{2}\text{j},\) where t measures time in seconds.
- Find \({a}_{\text{T}}\) and \({a}_{\text{N}}\) as functions of t.
- Find \({a}_{\text{T}}\) and \({a}_{\text{N}}\) at time \(t=-3.\)
Rivela la risposta
- \(\begin{array}{lll}\text{v}(t) & = & {r}^{'}(t)=4\text{i}+2t\ \text{j} \\ \text{a}(t) & = & {v}^{'}(t)=2\text{j} \\ {a}_{\text{T}} & = & \frac{2t}{\sqrt{{t}^{2}+4}},{a}_{\text{N}}=\frac{4}{\sqrt{4+{t}^{2}}}\end{array}\)
- \({a}_{\text{T}}(-3)=-\frac{6\sqrt{13}}{13},{a}_{\text{N}}(-3)=\frac{2\sqrt{13}}{13}\)
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During an Independence Day celebration, a cannonball is fired from a cannon on a cliff toward the water. The cannon is aimed at an angle of 30° above horizontal and the initial speed of the cannonball is \(600\ \text{ft/sec}\text{.}\) The cliff is 100 ft above the water ().
- Find the maximum height of the cannonball.
- How long will it take for the cannonball to splash into the sea?
- How far out to sea will the cannonball hit the water?
Rivela la risposta
We use the equation
\[\text{s}(t)={v}_{0}t\ \text{cos}\ \theta \ \text{i}+({v}_{0}t\ \text{sin}\ \theta -\frac{1}{2}g{t}^{2})\ \text{j}\]with \(\theta =30\text{^{\circ}},\) \(g=32{\ \text{ft/sec}}^{2},\) and \({v}_{0}=600\) ft/sec. Then the position equation becomes
\[\begin{array}{ll}\text{s}(t) & =600t(\text{cos}\ 30)\ \text{i}+(600t\ \text{sin}\ 30-\frac{1}{2}(32){t}^{2})\ \text{j} \\ & =300t\sqrt{3}\text{i}+(300t-16{t}^{2})\ \text{j}.\end{array}\]- The cannonball reaches its maximum height when the vertical component of its velocity is zero, because the cannonball is neither rising nor falling at that point. The velocity vector is
\[\begin{array}{ll}\text{v}(t) & ={s}^{'}(t) \\ & =300\sqrt{3}\text{i}+(300-32t)\ \text{j}.\end{array}\]
Therefore, the vertical component of velocity is given by the expression \(300-32t.\) Setting this expression equal to zero and solving for t gives \(t=9.375\) sec. The height of the cannonball at this time is given by the vertical component of the position vector, evaluated at \(t=9.375.\)
\[\begin{array}{ll}\text{s}(9.375) & =300(9.375)\sqrt{3}\text{i}+(300(9.375)-16{(9.375)}^{2})\ \text{j} \\ & =4871.39\text{i}+1406.25\text{j}\end{array}\]
Therefore, the maximum height of the cannonball is 1406.39 ft above the cannon, or 1506.39 ft above sea level. - When the cannonball lands in the water, it is 100 ft below the cannon. Therefore, the vertical component of the position vector is equal to \(-100.\) Setting the vertical component of \(\text{s}(t)\) equal to \(-100\) and solving, we obtain
\[\begin{array}{lll} \\ 300t-16{t}^{2} & = & -100 \\ 16{t}^{2}-300t-100 & = & 0 \\ 4{t}^{2}-75t-25 & = & 0 \\ t & = & \frac{75\pm \sqrt{{(-75)}^{2}-4(4)(-25)}}{2(4)} \\ & = & \frac{75\pm \sqrt{6025}}{8} \\ & = & \frac{75\pm 5\sqrt{241}}{8}.\end{array}\]
The positive value of t that solves this equation is approximately 19.08. Therefore, the cannonball hits the water after approximately 19.08 sec. - To find the distance out to sea, we simply substitute the answer from part (b) into \(\text{s}(t)\text{:}\)
\[\begin{array}{ll}\text{s}(19.08) & =300(19.08)\sqrt{3}\text{i}+(300(19.08)-16{(19.08)}^{2})\ \text{j} \\ & =9914.26\ \text{i}-100.7424\ \text{j}.\end{array}\]
Therefore, the ball hits the water about 9914.26 ft away from the base of the cliff. Notice that the vertical component of the position vector is very close to \(-100,\) which tells us that the ball just hit the water. Note that 9914.26 feet is not the true range of the cannon since the cannonball lands in the ocean at a location below the cannon. The range of the cannon would be determined by finding how far out the cannonball is when its height is 100 ft above the water (the same as the altitude of the cannon).
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An archer fires an arrow at an angle of 40° above the horizontal with an initial speed of 98 m/sec. The height of the archer is 171.5 cm. Find the horizontal distance the arrow travels before it hits the ground.
Rivela la risposta
967.15 m
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Kepler’s third law of planetary motion can be modified to the case of one object in orbit around an object other than the Sun, such as the Moon around the Earth. In this case, Kepler’s third law becomes
\[{P}^{2}=\frac{4{\pi }^{2}{a}^{3}}{G(m+M)},\]where m is the mass of the Moon and M is the mass of Earth, a represents the length of the major axis of the elliptical orbit, and P represents the period.
Given that the mass of the Moon is \(7.35\ \times \ {10}^{22}\ \text{kg,}\) the mass of Earth is \(5.97\ \times \ {10}^{24}\ \text{kg,}\) \(G=6.67\ \times \ {10}^{-11}{\text{m}}^{3}\text{/}\text{kg}\cdot {\text{sec}}^{2},\) and the period of the moon is 27.3 days, let’s find the length of the major axis of the orbit of the Moon around Earth.
Rivela la risposta
It is important to be consistent with units. Since the universal gravitational constant contains seconds in the units, we need to use seconds for the period of the Moon as well:
\[27.3\ \text{days}\ \times \ \frac{24\ \text{hr}}{1\ \text{day}}\ \times \ \frac{3600\ \text{sec}}{1\ \text{hour}}=2,358,720\ \text{sec}\text{.}\]Substitute all the data into and solve for a:
\[\begin{array}{lll}{(2,358,720\ \text{sec})}^{2} & = & \frac{4{\pi }^{2}{a}^{3}}{(6.67\ \times \ {10}^{-11}\ \frac{{\text{m}}^{3}}{\text{kg}\cdot \ {\text{sec}}^{2}})(7.35\ x\ {10}^{22}\text{kg}+5.97\ x\ {10}^{24}\text{kg})} \\ 5.563\ \times \ {10}^{12} & = & \frac{4{\pi }^{2}{a}^{3}}{(6.67\ \times \ {10}^{-11}\ {\text{m}}^{3})(6.04\ x\ {10}^{24})} \\ (5.563\ \times \ {10}^{12})(6.67\ \times \ {10}^{-11}\ {\text{m}}^{3})(6.04\ \times \ {10}^{24}) & = & 4{\pi }^{2}{a}^{3} \\ {a}^{3} & = & \frac{2.241\ \times \ {10}^{27}}{4{\pi }^{2}}{\text{m}}^{3} \\ a & = & 3.84\ \times \ {10}^{8}\text{m} \\ & \approx & 384,000\ \text{km.}\end{array}\] -
Titan is the largest moon of Saturn. The mass of Titan is approximately \(1.35\ \times \ {10}^{23}\) kg. The mass of Saturn is approximately \(5.68\ \times \ {10}^{26}\) kg. Titan takes approximately 16 days to orbit Saturn. Use this information, along with the universal gravitation constant \(G=6.67\ \times \ {10}^{-11}{\text{m}}^{3}\text{/}\text{kg}\cdot {\text{sec}}^{2}\) to estimate the distance from Titan to Saturn.
Rivela la risposta
\(a=1.224\ \times \ {10}^{9}\text{m}\approx 1,224,000\ \text{km}\)
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We now return to the chapter opener, which discusses the motion of Halley’s comet around the Sun. Kepler’s first law states that Halley’s comet follows an elliptical path around the Sun, with the Sun as one focus of the ellipse. The period of Halley’s comet is approximately 76.1 years, depending on how closely it passes by Jupiter and Saturn as it passes through the outer solar system. Let’s use \(T=76.1\) years. What is the average distance of Halley’s comet from the Sun?
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Using the equation \({T}^{2}={D}^{3}\) with \(T=76.1,\) we obtain \({D}^{3}=5791.21,\) so \(D\approx 17.96\) A.U. This comes out to approximately \(1.67\ \times \ {10}^{9}\) mi.
A natural question to ask is: What are the maximum (aphelion) and minimum (perihelion) distances from Halley’s Comet to the Sun? The eccentricity of the orbit of Halley’s Comet is 0.967 (Source: http://nssdc.gsfc.nasa.gov/planetary/factsheet/cometfact.html). Recall that the formula for the eccentricity of an ellipse is \(e=c\text{/}a,\) where a is the length of the semimajor axis and c is the distance from the center to either focus. Therefore, \(0.967=c\text{/}17.96\) and \(c\approx 17.37\) A.U. Subtracting this from a gives the perihelion distance \(p=a-c=17.96-17.37=0.59\) A.U. According to the National Space Science Data Center (Source: http://nssdc.gsfc.nasa.gov/planetary/factsheet/cometfact.html), the perihelion distance for Halley’s comet is 0.587 A.U. To calculate the aphelion distance, we add
\[P=a+c=17.96+17.37=35.33\ \text{A}\text{.U}\text{.}\]This is approximately \(3.3\ \times \ {10}^{9}\) mi. The average distance from Pluto to the Sun is 39.5 A.U. (Source: http://www.oarval.org/furthest.htm), so it would appear that Halley’s Comet stays just within the orbit of Pluto.
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Given \(\text{r}(t)=(3{t}^{2}-2)\text{i}+(2t-\text{sin}(t))\text{j},\) find the velocity of a particle moving along this curve.
Rivela la risposta
\(\text{v}(t)=(6t)\text{i}+(2-\text{cos}(t))\text{j}\)
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Given \(\text{r}(t)=(3{t}^{2}-2)\text{i}+(2t-\text{sin}(t))\text{j},\) find the acceleration vector of a particle moving along the curve in the preceding exercise.
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\(\text{r}(t)=〈3\ \text{cos}\ t,3\ \text{sin}\ t,{t}^{2}〉\)
Rivela la risposta
\(\text{v}(t)=〈-3\ \text{sin}\ t,3\ \text{cos}\ t,2t〉,\) \(\text{a}(t)=〈-3\ \text{cos}\ t,-3\ \text{sin}\ t,2〉,\) \(\text{speed}=\sqrt{9+4{t}^{2}}\)
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\(\text{r}(t)={e}^{\text{-}t}\text{i}+{t}^{2}\text{j}+\text{tan}\ t\ \text{k}\)
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\(\text{r}(t)=2\ \text{cos}\ t\ \text{j}+3\ \text{sin}\ t\ \text{k}.\)
Rivela la risposta
\(v(t)=-2\sin \ t\ j+3\ \cos \ t\ k,\) \(\text{a}(t)=-2\ \text{cos}\ t\ \text{j}-3\ \text{sin}\ t\ \text{k},\) \(\text{speed}=\sqrt{4\ {\text{sin}}^{2}t+9{\text{cos}}^{2}t}\)
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\(\text{r}(t)=〈{t}^{2}-1,t〉\)
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\(\text{r}(t)=〈{e}^{t},{e}^{\text{-}t}〉\). The graph is shown here:
Rivela la risposta
\(\text{v}(t)={e}^{t}\text{i}-{e}^{\text{-}t}\text{j},\) \(\text{a}(t)={e}^{t}\text{i}+{e}^{\text{-}t}\text{j},\) speed = \(‖\text{v}(t)‖=\sqrt{{e}^{2t}+{e}^{-2t}}\)
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\(\text{r}(t)=〈\text{sin}\ t,t,\text{cos}\ t〉.\)
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The position function of an object is given by \(\text{r}(t)=〈{t}^{2},5t,{t}^{2}-16t〉.\) At what time is the speed a minimum?
Rivela la risposta
\(t=4\)
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Let \(\text{r}(t)=r\ \text{cosh}(\omega t)\text{i}+r\ \text{sinh}(\omega t)\text{j}.\) Find the velocity and acceleration vectors and show that the acceleration is proportional to \(\text{r}(t).\)
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Find the equations for the velocity, acceleration, and speed of the particle at any time.
Rivela la risposta
\(\text{v}(t)=(\omega -\omega \ \text{cos}(\omega t))\ \text{i}+(\omega \ \text{sin}(\omega t))\ \text{j},\)
\(\text{a}(t)=({\omega }^{2}\text{sin}(\omega t))\ \text{i}+({\omega }^{2}\text{cos}(\omega t))\ \text{j},\)
\(\text{speed}=\sqrt{{\omega }^{2}-2{\omega }^{2}\text{cos}(\omega t)+{\omega }^{2}{\text{cos}}^{2}(\omega t)+{\omega }^{2}{\text{sin}}^{2}(\omega t)}\ \text{=}\ \sqrt{2{\omega }^{2}(1-\text{cos}(\omega t))}\) -
The velocity and acceleration vectors
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The glider’s speed at any time
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\(‖\text{v}(t)‖=\sqrt{9+4{t}^{2}}\)
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The times, if any, at which the glider’s acceleration is orthogonal to its velocity
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The velocity of the particle
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\(\text{v}(t)=〈{e}^{-5t}(\text{cos}\ t-5\ \text{sin}\ t),\text{-}{e}^{-5t}(\text{sin}\ t+5\ \text{cos}\ t),-20{e}^{-5t}〉\)
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The speed of the particle
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The acceleration of the particle
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\(\text{a}(t)={〈e}^{-5t}(\text{-}\text{sin}\ t-5\ \text{cos}\ t)-5{e}^{-5t}(\text{cos}\ t-5\ \text{sin}\ t),\) \(\text{-}{e}^{-5t}(\text{cos}\ t-5\ \text{sin}\ t)+5{e}^{-5t}(\text{sin}\ t+5\ \text{cos}\ t),100{e}^{-5t}〉\)
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Find the maximum speed of a point on the circumference of an automobile tire of radius 1 ft when the automobile is traveling at 55 mph.
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At what time does the projectile reach maximum height?
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44.185 sec
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What is the approximate maximum height of the projectile?
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At what time is the maximum range of the projectile attained?
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\(t=88.37\) sec
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What is the maximum range?
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What is the total flight time of the projectile?
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88.37 sec
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Determine the maximum height of the projectile.
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Determine the range of the projectile.
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The range is approximately 886.29 m.
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A golf ball is hit in a horizontal direction off the top edge of a building that is 100 ft tall. How fast must the ball be launched to land 450 ft away?
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A projectile is fired from ground level at an angle of 8° with the horizontal. The projectile is to have a range of 50 m. Find the minimum velocity necessary to achieve this range.
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\(\text{v}=42.16\) m/sec
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Prove that an object moving in a straight line at a constant speed has an acceleration of zero.
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The acceleration of an object is given by \(\text{a}(t)=t\ \text{j}+t\ \text{k}.\) The velocity at \(t=1\) sec is \(\text{v}(1)=5\text{j}\) and the position of the object at \(t=1\) sec is \(\text{r}(1)=0\text{i}+0\text{j}+0\text{k}.\) Find the object’s position at any time.
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\(\text{r}(t)=0\text{i}+(\frac{1}{6}{t}^{3}+4.5t-\frac{14}{3})\ \text{j}+(\frac{{t}^{3}}{6}-\frac{1}{2}t+\frac{1}{3})\ \text{k}\)
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Find \(\text{r}(t)\) given that \(\text{a}(t)=-32\text{j},\) \(\text{v}(0)=600\sqrt{3}\text{i}+600\text{j},\) and \(\text{r}(0)=0.\)
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Find the tangential and normal components of acceleration for \(\text{r}(t)=a\ \text{cos}(\omega t)\text{i}+a\ \text{sin}(\omega t)\text{j}\) at \(t=0.\)
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\({a}_{T}=0,\) \({a}_{N}=a{\omega }^{2}\)
Symbols used here
Antiderivative (indefinite) or signed area from a to b (definite).
The non-negative number whose square (n-th power) is x.
Ratio of a circle's circumference to its diameter, 3.14159…
Instantaneous rate of change; slope of the graph.
i² = −1.
Derivative with respect to x, holding the other variables fixed.
Vector of partial derivatives; points uphill.
Integral over a region of the plane; integral around a closed curve.
A quantity with magnitude and direction; a column of numbers.
Σ u_i v_i; the length of v, √(v·v).
How to: Motion in Space
- Describe the velocity and acceleration vectors of a particle moving in space.
- Explain the tangential and normal components of acceleration.
- State Kepler’s laws of planetary motion.
- Find the velocity, acceleration, and speed as functions of time.
- Sketch the curve along with the velocity vector at time
- We use
- The graph of
- Find
Questions people ask
What is a partial derivative?
The ordinary derivative with respect to one variable while every other variable is frozen — the slope of the surface in one coordinate direction.
What does the gradient point at?
Uphill: the direction of steepest increase, with length equal to that steepest slope. It is perpendicular to the level curves.
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Parts of this page are adapted from OpenStax Calculus Volume 3 (CC BY-NC-SA 4.0). Condensed and re-explained here; errors are ours.
Più in Multivariable Calculus
Functions of several variablesPartial derivatives and the gradientOptimisation in several variablesDouble and triple integralsVector fields, line integrals and the big theorems