DocumentCode :
3350783
Title :
A Reentry Trajectory Planning Based on the Optimization of Angle of Attack
Author :
Zhuo, Yang ; Qingzhen, Zhang ; Xiaoqiang, Tao
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., BeiHang Univ., Beijing, China
fYear :
2011
fDate :
21-23 Oct. 2011
Firstpage :
937
Lastpage :
940
Abstract :
According to the strict aerodynamic heating environment in the reentry process, a new reentry trajectory planning method is presented. A reasonable Heat Flux Rate (HFR) curve is designed with the energy of the aircraft, and the real-time instruction of the Angle of Attack (AOA) is decoded. Then, the flight corridor is planned by the multi-constraint conditions. After that, the flight trajectory could be optimized through applying the pseudo-spectral method. At last, the simulation experiment under Matlab is carried out with an example lifting flight. The results show that the aircraft´s total heat absorption (THA), which got through the new planning method, is smaller than that by the traditional method.
Keywords :
absorption; aerodynamics; aircraft; planning; Matlab; aerodynamic heating environment; aircraft total heat absorption; angle of attack optimization; flight corridor; flight trajectory; heat flux rate curve; lifting flight; pseudo-spectral method; reentry trajectory planning method; Aircraft; Heating; Optimization; Planning; Real time systems; Trajectory; Vehicles; angle of attack (AOA); heat flux rate (HFR); lifting flight; reentry; trajectory planning;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control, 2011 First International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-0-7695-4519-6
Type :
conf
DOI :
10.1109/IMCCC.2011.236
Filename :
6154262
Link To Document :
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