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Lesson Directive // Derivatives & Rate of ChangeREF_CORE

Instantaneous Change

v(t)v(t)==dddtdts(t)s(t)

Hover over a variable in the formula above, or see glossary below:

v(t)v(t)
Velocity
m/s
s(t)s(t)
Position Function
m
tt
Time
s

While algebra gives average speed over a long trip, calculus allows us to find the exact velocity of a spacecraft at a single instant in time. This is the foundation for solving complex Differential Equations.

INSIGHT: A derivative is simply a rate of change at a specific moment.

The Derivative

Taking the derivative of a position function gives the velocity function. Taking the derivative of velocity gives acceleration. These precise calculations allow us to model complex Trajectories.

INSIGHT: Position -> Velocity -> Acceleration.

Rocket Trajectories

As a rocket burns fuel, its mass changes constantly, and its acceleration increases. Calculus is essential to model these dynamic, continuously changing systems.

INSIGHT: Calculus helps predict complex, changing motion.
Detailed Theory & ReferencesEXT_DOC

Differential Calculus and Rates of Change

Calculus, independently developed by Isaac Newton and Gottfried Wilhelm Leibniz in the late 17th century, is the mathematical study of continuous change. Differential calculus focuses on the concept of the derivative, which measures the instantaneous rate of change of a quantity with respect to another.

The Derivative

If a function s(t)s(t) represents the position of an object moving along a line at time tt, the average velocity over a time interval Δt\Delta t is ΔsΔt\frac{\Delta s}{\Delta t}. The instantaneous velocity v(t)v(t) is defined as the limit of this average velocity as the time interval approaches zero: v(t)=lim⁡Δt→0s(t+Δt)−s(t)Δt=dsdtv(t) = \lim_{\Delta t \to 0} \frac{s(t + \Delta t) - s(t)}{\Delta t} = \frac{ds}{dt}

Higher-Order Derivatives

Derivatives can themselves be differentiated. Acceleration a(t)a(t) is the rate of change of velocity, and therefore the second derivative of position: a(t)=dvdt=d2sdt2a(t) = \frac{dv}{dt} = \frac{d^2s}{dt^2}

Numerical Integration (Euler's Method)

In computational physics, analytical solutions to complex differential equations (like chaotic multi-body gravitational systems) are often impossible. Instead, algorithms perform numerical integration to approximate the solution over small discrete time steps (Δt\Delta t).

Euler's method is the simplest first-order numerical procedure: s(tn+1)≈s(tn)+v(tn)Δts(t_{n+1}) \approx s(t_n) + v(t_n) \Delta t v(tn+1)≈v(tn)+a(tn)Δtv(t_{n+1}) \approx v(t_n) + a(t_n) \Delta t

While Euler's method provides the foundation for understanding computational integration, modern spacecraft simulators utilise more stable and accurate higher-order algorithms like Runge-Kutta (RK4) to minimize accumulated truncation errors over time.

Reference: Stewart, J. (2015). Calculus: Early Transcendentals (8th ed.). Cengage Learning.

References

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