Improved tentacle-based method based on approximate analysis for entry flight

被引:0
|
作者
Zhu Yichuan [1 ]
Ling, Li [2 ]
Rui, Mu [3 ]
机构
[1] Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence C, Beijing, Peoples R China
[2] Natl Key Lab Sci & Technol Aerosp Intelligence Co, Comm Sci & Technol, Beijing, Peoples R China
[3] Beijing Aerocim Technol Co, Software Lab, Beijing, Peoples R China
关键词
Gliding aircraft; Maneuver guidance; Tentacle-based method; Approximate analytical solution;
D O I
10.1109/CCDC58219.2023.10327370
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Aiming at the no-fly zone constraint in the process of aircraft gliding reentry, this paper presents an improved strategy for tentacle-based detection. The turning radius and reference pitch angle of the aircraft can be obtained by approximate analytical solution and then the waypoint can be obtained according to geometric relationship. Next tentacle-based method is used to correct the trajectory to meet the flight requirements. By approximate analytical solution programming, the number of tentacles required can be reduced, and the influence of integration process on the calculation efficiency can be reduced, thus the calculation time can be shortened effectively. After the no-fly zone is bypassed, height planning is performed to meet the terminal height constraints. The simulation results show that this method can effectively avoid the no-fly zone and satisfy various constraints of gliding reentry process, and The calculation time is shortened to 22.24%.
引用
收藏
页码:1188 / 1194
页数:7
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