Title :
Design of Autopilot for Aerodynamic/Reaction-Jet Multiple Control Missile
Author :
Sui, Qi SHeng ; Li, Xin ; Fan, Yong Hua
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an
Abstract :
A new scheme of reaction-jet/aerodynamic multi-control missile using pose controlled pulse-engine is present. In this scheme, aerodynamic is used as feedback control, and reaction-jet is feed-forward control. In the first part, the model of the multi-control system is given; then, the aerodynamic controller is designed by using pole assignment, and the reaction-jet controller has been designed by using the term of entirely compensated. Finally it has been proved by simulation that this multiple controller can greatly enhance response speed and the scheme is feasible.
Keywords :
aerodynamics; control system synthesis; feedback; feedforward; jet engines; missile control; pole assignment; aerodynamic multicontrol missile; autopilot; feed-forward control; feedback control; pole assignment; pose controlled pulse-engine; reaction-jet multiple control missile; Aerodynamics; Automatic control; Control systems; Educational institutions; Engines; Equations; Feedback control; Feedback loop; Feedforward systems; Missiles;
Conference_Titel :
Intelligent Computation Technology and Automation (ICICTA), 2008 International Conference on
Conference_Location :
Hunan
Print_ISBN :
978-0-7695-3357-5
DOI :
10.1109/ICICTA.2008.101
