An attempt at implementing the function that approximates the apogee of the rocket using the kinetics model. Equations used are from MODELING MODEL ROCKETS: A STUDY IN OPTIMIZING MODEL ROCKETRY but adapted to be in 3-space instead of just the vertical axis
An attempt at implementing the function that approximates the apogee of the rocket using the kinetics model. Equations used are from MODELING MODEL ROCKETS: A STUDY IN OPTIMIZING MODEL ROCKETRY but adapted to be in 3-space instead of just the vertical axis
Math reference (pg. 8)
Missing: