DocumentCode
3092516
Title
Solution for trajectory correction optimization based on generalized work principle
Author
Yao, Jun ; Wang, Xin ; Wang, Xiaobo
Author_Institution
Shenyang Ligong Univ., Shenyang, China
fYear
2010
fDate
15-17 June 2010
Firstpage
797
Lastpage
801
Abstract
A optimization control method based on generalized work minimum principle is presented to solve the optimization control problems in trajectory correction projectiles. The optimal control problem is addressed through an optimization control strategy with the aim of the smallest undershoot and the minimum energy. On the condition of fixed starting point and fixed terminal point, optimal solutions are obtained and a simulating example is demonstrated. The simulation results show that the trajectory correction optimal values can control the trajectory correction projectiles through trajectory correction actuator to hit the target with the smallest undershoot and the minimum energy. The results are rather satisfactory, which shows that optimization control method has excellent performance of optimization and may be taken as a practical algorithm for design of the trajectory correction actuator.
Keywords
aerospace control; minimisation; optimal control; position control; projectiles; fixed starting point condition; fixed terminal point condition; generalized work minimum principle; optimal control; optimization control; trajectory correction projectiles; Actuators; Computational modeling; Design optimization; Equations; Optimal control; Optimization methods; Power engineering computing; Projectiles; Trajectory; Weather forecasting; generalized work principle; optimization control; simulation; trajectory correction;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications (ICIEA), 2010 the 5th IEEE Conference on
Conference_Location
Taichung
Print_ISBN
978-1-4244-5045-9
Electronic_ISBN
978-1-4244-5046-6
Type
conf
DOI
10.1109/ICIEA.2010.5515077
Filename
5515077
Link To Document