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.


Inertial Measurement Unit Control Torque Launch Vehicle Pitching Moment Sideslip Angle 
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Copyright information

© Springer Science+Business Media, LLC 2011

Authors and Affiliations

  1. 1.Department of Aerospace EngineeringIndian Institute of TechnologyKanpurIndia

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