Autonomous Navigation and Guidance for Change-3 Soft Landing

HUANG Xiangyu1, ZHANG Honghua2, WANG Datie3, LI Ji4, GUAN Yifeng5, WANG Pengji6

PDF(1413 KB)
PDF(1413 KB)
Journal of Deep Space Exploration ›› 2014, Vol. 1 ›› Issue (1) : 52-59.
Article
Article

Autonomous Navigation and Guidance for Change-3 Soft Landing

  • HUANG Xiangyu1, ZHANG Honghua2, WANG Datie3, LI Ji4, GUAN Yifeng5, WANG Pengji6
Author information +
History +

Abstract

Chang' e-3 implemented its soft landing on the moon which is the first time for a Chinese spacecraft to conduct soft landing on an extraterrestrial body. GNC is the key to achieve successful soft landing. For the desire of high safe and reliable soft landing, the soft landing flight program including rough-fine-relay hazard avoidance is designed, the autonomous navigation method based on single beam time-sharing correction and multi-beams fusion filter, and the self-adaption powered explicit guidance, the non-iteration polynomial large hazard avoidance guidance, the inner-outer-loop small hazard avoidance guidance are presented. The real flight result of Chang' e-3 shows integration that the high-precision states is estimated by navigation algorithm, the high-precision states control and effective hazard avoidance maneuver areimplemented by guidance algorithm to ensure the safety and reliability for lunar soft landing.

Keywords

Chang' e-3 / soft landing / autonomous navigation / guidance

Cite this article

Download citation ▾
HUANG Xiangyu, ZHANG Honghua, WANG Datie, LI Ji, GUAN Yifeng, WANG Pengji. Autonomous Navigation and Guidance for Change-3 Soft Landing. Journal of Deep Space Exploration, 2014, 1(1): 52‒59

References

[1] Klumpp A R. Apollo guidance, naivgation and control[R].NASA R一695,1971.
[2] Thomas F. Lunar landing and ascent trajectory guidance design for the autonomous landing and hazard avoidance technology (ALHAT) program[J].Advances in the Astronautical Sciences,2010, 136:2317-2336.
[3] Savage P G. Strapdown inertial navigation integration algorithm design part 1:attitude algorithms[J].Journal of Guidance,Control and Dynamics, 1998, 21(1):19-28.
[4] Savage P G. Strapdown inertial navigation integration algorithm design part 2; velocity and position algorithms[J].Journal of Guidance, Control and Dynamics, 1998,21(2):208-221.
[5] McHenry R L, Brand T J, Long A D, et al.Space shuttle ascent guidance, navigation, and contml[J].The Journal of the Astronautical Sciences, 1979, 27(1);1-38.
[6] Klumpp A R. Apollo lunar descent guidance[J].Automatica, 1974, 10; 133-146.
[7] 屠善澄.卫星姿态动力学与控制[M].北京:中国宇航出版社,1998:168-175.[Tu S C. The satellite attitude dynamics and control[M]. Beijing; China Astronautic Publishing House,1998:168-175.]
PDF(1413 KB)

Accesses

Citations

Detail

Sections
Recommended

/