DocumentCode
2526143
Title
Research on the method of target reconstruction guidance
Author
Yuqiu, Huang ; Linshu, He
Author_Institution
Sch. of Astronaut., BeiHang Univ., Beijing, China
fYear
2011
fDate
23-25 May 2011
Firstpage
4369
Lastpage
4373
Abstract
According to the application of unpowered reentry vehicle, a guidance method which is suitable for on-board target reconstruction is studied and analyzed in detail. Then, the longitudinal and lateral guidance laws are designed based on the reentry flight model and the dynamic response to guidance commands. A simulation of on-board target reconstruction is performed according to typical reentry trajectory. Simulation results show that the guidance algorithm is effective and accurate. The guidance method is feasible and validated for lifting reentry vehicle.
Keywords
command and control systems; missile guidance; space vehicles; flight model; guidance algorithm; guidance commands; lateral guidance laws; longitudinal guidance laws; onboard target reconstruction; target reconstruction guidance method; unpowered reentry vehicle application; Acceleration; Algorithm design and analysis; Earth; Space shuttles; Trajectory; Vehicle dynamics; Lifting Reentry Vehicle; Reentry Guidance; Target Reconstruction;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2011 Chinese
Conference_Location
Mianyang
Print_ISBN
978-1-4244-8737-0
Type
conf
DOI
10.1109/CCDC.2011.5968996
Filename
5968996
Link To Document