DocumentCode
2849727
Title
A re-entry guidance method for vehicle using virtual displacement concept
Author
Gao, Changsheng ; Li, Ruikang ; Jing, Wuxing
Author_Institution
Dept. of Aerosp. Eng., Harbin Inst. of Technol., Harbin, China
fYear
2010
fDate
26-28 May 2010
Firstpage
579
Lastpage
582
Abstract
A new guidance law for reentry vehicle is presented in this paper. The proposed approach is based on the fact that lateral force is formed in a plane which is perpendicular to the reentry vehicle velocity. Particularly, the nominal impact point is defined as the impact point generated by zero lift trajectory. The virtual displacement is defined as the tiny change of the nominal impact point, which is caused by any instantaneous lateral force at the beginning of the trajectory. The optimal direction of the lateral force is obtained by the solution of optimal virtual displacement, in which the optimal virtual displacement should point to the target. The analytical solution of reentry trajectory and the linear quadratic gauss (LQG) method are used to design this guidance law. The simulation results demonstrate the effectiveness of the proposed method.
Keywords
Gaussian processes; aerospace control; displacement control; motion control; position control; lateral force; linear quadratic Gauss method; nominal impact point; reentry guidance method; reentry trajectory; reentry vehicle; virtual displacement; zero lift trajectory; Analytical models; Computer errors; Equations; Feedback; Gaussian processes; Navigation; Predictive models; Trajectory; Upper bound; Vehicles; Analytical Solution; Guidance Law; LQG; Reentry Vehicle; Virtual Displacement;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2010 Chinese
Conference_Location
Xuzhou
Print_ISBN
978-1-4244-5181-4
Electronic_ISBN
978-1-4244-5182-1
Type
conf
DOI
10.1109/CCDC.2010.5498983
Filename
5498983
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