$$\frac{\partial V}{\partial t} + \frac{1}{2}\sigma^2 S^2 \frac{\partial^2 V}{\partial S^2} = rV - rS \frac{\partial V}{\partial S}$$  Rocket transfer function

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Learn the fundamentals of building a rocket control system using basic control theory and Python. The guide explores crucial concepts such as PID controllers, transfer functions, and stability analysis using root locus, Bode plots, and Nyquist plots. A step-by-step code example demonstrates the implementation of a PID controller to maintain stability and control of the rocket's trajectory.

How to Build a Rocket Control System: Basic Control Theory with Python

Rocket Systems and Cake Baking: A Fun Comparison

Rocket Control Made Simple: Understanding PID Controllers

Code example: Designing a simple PID controller

<p>Now do it with KRPC and Kerbal Space Program like I did. Your code actually works with the correct streams and controls. Takes only a little more code to get a stable orbit. Easy enough to fly it up there with what you’ve provided on PIDs though.</p>
