Asteroid Landing Trajectory Dynamic Planning Method with Complex Topography Adaptability

GE Dantong1,2,3, ZHU Shengying1,2,3

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PDF(898 KB)
Journal of Deep Space Exploration ›› 2021, Vol. 8 ›› Issue (2) : 132-139. DOI: 10.15982/j.issn.2096-9287.2021.20200072
Topic:Autonomous Planning Technology for Deep Space Exploration

Asteroid Landing Trajectory Dynamic Planning Method with Complex Topography Adaptability

  • GE Dantong1,2,3, ZHU Shengying1,2,3
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Abstract

Considering the safety threats posed by the complicated topography on the asteroid surface,a dynamic planning method for topography-adaptive landing trajectory is proposed. In this paper,a multi-objective optimal waypoint sequence is developed for the landing process. Based on the hazard detection information,an online evaluation of the collision threats is carried out. To solve the conflicts between hazards and the nominal trajectory,a minimum waypoint re-planning method is designed,which realizes an autonomous switch between waypoint robust tracking and dynamic planning of the local hazard avoidance trajectory during descent. By employing the proposed method,adaptability to the complex topography environment of the lander is enhanced and the asteroid landing mission safety is improved.

Keywords

asteroid landing / complicated topography / waypoint planning / multi-objective optimization / environment adaptability

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GE Dantong, ZHU Shengying. Asteroid Landing Trajectory Dynamic Planning Method with Complex Topography Adaptability. Journal of Deep Space Exploration, 2021, 8(2): 132‒139 https://doi.org/10.15982/j.issn.2096-9287.2021.20200072

References

[1] OGAWA N,TERUI F,YASUDA S,et al. Image-based autonomous navigation of Hayabusa2 using artificial landmarks:design and in-flight results in landing operations on asteroid Ryugu[C]//AIAA SCITECH 2020 Forum. [S. l.]:AIAA,2020.
[2] EVERETT D,MINK R,LINN T,et al. Designing to sample the unknown:lessons from OSIRIS-REx project systems engineering[C]//2017 IEEE Aerospace Conference. [S. l.]:IEEE,2017.
[3] 崔平远,葛丹桐,朱圣英,等. 行星着陆点自主评估与选取研究进展[J]. 中国科学:技术科学,DOI:10.1360/SST-2020-0228.
[4] BIELE J,ULAMEC S,MAIBAUM M,et al. The landing(s) of Philae and inferences about comet surface mechanical properties[J]. Science,2015,349:6247.
[5] YOSHIKAWA K,KIKUCHI S,SAWADA H,et al. Hayabusa 2 spacecraft dynamics and operational design of final descent and touchdown in sampling mission[C]//AIAA SCITECH 2020 Forum. [S. l.]:AIAA,2020.
[6] 于洋,宝音贺西. 小天体附近的轨道动力学研究综述[J]. 深空探测学报(中英文),2014,1(2):93-104
YU Y,BAOYIN H X. Review of orbital dynamics in the vicinity of solar system small celestial bodies scientific vision for future missions[J]. Journal of Deep Space Exploration,2014,1(2):93-104
[7] 袁旭,朱圣英,乔栋,等. 小天体着陆动力学参数不确定性影响分析[J]. 深空探测学报(中英文),2014,1(2):134-139
YUAN X,ZHU S Y,QIAO D,et al. Impact analysis of dynamic parameters uncertainty on small celestial body landing[J]. Journal of Deep Space Exploration,2014,1(2):134-139
[8] KAWAGUCHI J,FUJIWARA A,UESUGI T. Hayabusa—its technology and science accomplishment summary and Hayabusa-2[J]. Acta Astronautica,2008,62(10-11):639-647
[9] YANG H W,BAI X L,BAOYIN H X. Rapid generation of time-optimal trajectories for asteroid landing via convex optimization[J]. Journal of Guidance Control Dynamics,2017,40(3):628-641
[10] LEE U,MESBAHI M. Constrained autonomous precision landing via dual quaternions and model predictive control[J]. Journal of Guidance,Control,and Dynamics,2017,40(2):292-308
[11] GUI H,VUKOVICH G. Robust adaptive tracking of rigid body motion with applications to asteroid proximity operations[J]. IEEE Transactions on Aerospace and Electronic Systems,2017,53(1):419-430
[12] 袁旭,朱圣英,崔平远. 小天体自主附着多滑模面鲁棒制导方法研究[J]. 深空探测学报(中英文),2015,2(4):345-351
YUAN X,ZHU S Y,CUI P Y. Study on robust multiple sliding surface guidance method for autonomous small celestial body landing[J]. Journal of Deep Space Exploration,2015,2(4):345-351
[13] GE D T,CUI P Y,ZHU S Y. Recent development of autonomous GNC technologies for small celestial body descent and landing[J]. Progress in Aerospace Sciences,2019,110:100551
[14] STENTZ A. Optimal and efficient path planning for partially-known environments[C]//IEEE International Conference on Robotics and Automation. [S. l.]:IEEE,1994.
[15] KOENIG S,LIKHACHEV M. Fast replanning for navigation in unknown terrain[J]. IEEE Transactions on Robotics,2005,21(3):354-363
[16] 黄鲁,周非同. 基于路径优化D*Lite算法的移动机器人路径规划[J]. 控制与决策,2020,35(4):877-884
HUANG L,ZHOU F T. Path planning of moving robot based on path optimization of D* Lite algorithm[J]. Control and Decision,2020,35(4):877-884
[17] LU P. Theory of fractional-polynomial powered descent guidance[J]. Journal of Guidance,Control,and Dynamics,2020,43(3):398-409
[18] CUI P Y,QIN T,ZHU S Y,et al. Trajectory curvature guidance for Mars landings in hazardous terrains[J]. Automatica,2018,93:161-171
[19] DUERI D,BEH?ET A,SCHARF D P,et al. Customized real-time interior-point methods for onboard powered-descent guidance[J]. Journal of Guidance Control and Dynamics,2016,40(2):197-212
[20] LI T,LONGMAN R W. Designing iterative learning control of non-minimum phase systems to converge to zero tracking error[C]//AIAA/AAS Astrodynamics Specialist Conference. [S. l.]:AIAA,2017.
[21] WERNER R A,SCHEERES D J. Exterior gravitation of a polyhedron derived and compared with harmonic and mascon gravitation representations of Asteroid 4769 Castalia[J]. Celestial Mechanics and Dynamical Astronomy,1996,65(3):313-344
[22] YUAN X,YU Z S,CUI P Y,et al. Probability-based hazard avoidance guidance for planetary landing[J]. Acta Astronautica,2018,144:12-22
[23] 王汀,郭延宁,张瑶,等. 基于模型预测控制的多约束火星精确着陆制导律研究[J]. 深空探测学报(中英文),2016,3(4):377-383
WANG T,GUO Y N,ZHANG Y,et al. Model predictive control guidance for constrained Mars pinpoint landing[J]. Journal of Deep Space Exploration,2016,3(4):377-383
[24] EREN U,PRACH A,KOCER B,et al. Model predictive control in aerospace systems:current state and opportunities[J]. Journal of Guidance,Control,and Dynamics,2017,40(7):1541-1566
[25] GAL-EDD J,CHEUVRONT A. The OSIRIS-REx asteroid sample return mission operations design[C]//13th International Conference on Space Operations. Pasadena,CA:[s. n.],2014.
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