DocumentCode
1654184
Title
Optimal Guidance Law Design for Reentry Vehicle Using Virtual Displacement Concept
Author
Changsheng, Gao ; Wuxing, Jing ; Chaoyong, Li
Author_Institution
Harbin Inst. of Technol., Harbin
fYear
2007
Firstpage
507
Lastpage
510
Abstract
The new predictive guidance law for reentry vehicle is presented in this paper. The proposed approach is based on the fact that lateral forces are formed to a plane perpendicular to the reentry vehicle velocity. In particular, the nominal ground location is defined as the ground location generated by the zero lift trajectory, the virtual displacement is defined as the small changes of the nominal ground location, this changes is caused by any instantaneous lateral force at the beginning of the trajectory. The optimal direction of the lateral force is searched by the solution to the optimal virtual displacement, in which case the virtual displacement is pointing to the target ground location. The analytical solution to the reentry trajectory and the linear quadratic Gauss (LQG) method are used in this guidance method. The simulation results show that the effectiveness of proposed method.
Keywords
aircraft control; linear quadratic Gaussian control; predictive control; linear quadratic gauss method; nominal ground location; optimal guidance law design; optimal virtual displacement; predictive guidance law; reentry vehicle velocity; virtual displacement concept; zero lift trajectory; Aerospace control; Aircraft; Displacement control; Equations; Gaussian processes; Land vehicles; Navigation; Optimal control; Road vehicles; Trajectory; Optimal; guidance law; linear quadratic gauss; reentry vehicle; virtual displacement;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference, 2007. CCC 2007. Chinese
Conference_Location
Hunan
Print_ISBN
978-7-81124-055-9
Electronic_ISBN
978-7-900719-22-5
Type
conf
DOI
10.1109/CHICC.2006.4347462
Filename
4347462
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