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Topic:Autonomous Planning Technology for Deep Space Exploration
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
Author information
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1. Institute of Deep Space Exploration,Beijing Institute of Technology,Beijing 100081,China;
2. Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology,Beijing 100081,China;
3. Key Laboratory of Dynamics and Control of Flight Vehicle,Ministry of Education,Beijing 100081,China
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History
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Received |
Revised |
Published |
03 Nov 2020 |
04 Dec 2020 |
20 Apr 2021 |
Issue Date |
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20 Apr 2021 |
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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.