Acta Aeronautica et Astronautica Sinica ›› 2023, Vol. 44 ›› Issue (23): 628483-628483.doi: 10.7527/S1000-6893.2023.28483
• Special Topic: Reusable Launch Vehicle Technology • Previous Articles Next Articles
Zhi ZHANG1(), Han YUAN2, Wanqing ZHANG2
Received:
2023-01-09
Revised:
2023-02-15
Accepted:
2023-07-11
Online:
2023-12-15
Published:
2023-09-13
Contact:
Zhi ZHANG
E-mail:Zhangzh2015V@sina.cn
CLC Number:
Zhi ZHANG, Han YUAN, Wanqing ZHANG. Powered deceleration guidance method based on gravity-turn analytical solutions[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(23): 628483-628483.
Table 2
Two cases of nominal return trajectory (in landing coordinate system)
参数 | 一二级分离 | 发动机开机 | 发动机关机 | |
---|---|---|---|---|
算例1 | x0/m | -493 736 | -86 673 | -55 202 |
y0/m | 47 886 | 65 343 | 48 047 | |
z0/m | -20 522 | -3 740 | -2 359 | |
vx,0/(m·s-1) | 1 798.8 | 1 887.7 | 1 239.0 | |
vy,0/(m·s-1) | 1 098.4 | -939.7 | -766.2 | |
vz,0/(m·s-1) | 62.0 | 83.1 | 54.1 | |
m0/kg | 84 000 | 84 000 | 67 091 | |
算例2 | x0/m | -333 886 | -78 932 | -69 043 |
y0/m | 49 403 | 66 181 | 60 720 | |
z0/m | -11 662 | -2 843 | -2 477 | |
vx,0/(m·s-1) | 1 381.3 | 1 431.0 | 1 168.2 | |
vy,0/(m·s-1) | 941.0 | -753.8 | -679.5 | |
vz,0/(m·s-1) | 39.6 | 53.0 | 43.2 | |
m0/kg | 73 500 | 73 500 | 67 075 |
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