Automatic Control of Rockets
Part of the Control Engineering book series (CONTRENGIN)
To model a rocket’s attitude plant with gimbaled nozzle and reaction jet actuators. To design and analyze a rocket’s roll, pitch, and yaw control systems using single-variable and multi-variable methods.
KeywordsInertial Measurement Unit Control Torque Launch Vehicle Pitching Moment Sideslip Angle
© Springer Science+Business Media, LLC 2011