Title :
The Switch Time Simulation of a Kind of Jet Element and its Effect on Control Precision
Author :
Ma, Wuju ; Yao, Xiaoxian ; Cheng, Jianwei
Author_Institution :
Sch. of Aerosp. Sci., Beijing Inst. of Technol., Beijing, China
Abstract :
Rocket missile is an important weapon for saturation attack, which exist the problem of the precision. In order to improve the bad precision, the facility control is added. Jet element is the key actuating mechanism of the attitude control for rocket missile. The switch time of jet element is critical for control precision, in this paper the switch time is simulated and its effect on control precision is discussed. The right time when the control system produces control signal is given. Finally, the simulation of trajectory shows that trajectory correction with jet element in side direction is feasible.
Keywords :
attitude control; jets; missile control; position control; rockets; actuating mechanism; attitude control; control signal; jet element; precision control; rocket missile; saturation attack; switch time simulation; trajectory correction; Computational modeling; Control systems; Equations; Force control; Missiles; Plugs; Rockets; Spinning; Switches; Testing; Jet element; simulation and test; the switch time;
Conference_Titel :
Intelligent Computation Technology and Automation (ICICTA), 2010 International Conference on
Conference_Location :
Changsha
Print_ISBN :
978-1-4244-7279-6
Electronic_ISBN :
978-1-4244-7280-2
DOI :
10.1109/ICICTA.2010.204
