NAVIGATION

作品数：641被引量：1385H指数：17
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Feasibility analysis of angles-only navigation algorithm with multisensor data fusion for spacecraft noncooperative rendezvous被引量：2
《Astrodynamics》2023年第2期179-196,共18页Ronghua Du Wenhe Liao Xiang Zhang 
supported by the China Aerospace Science and Technology Corporation Eighth Research Institute Industry-University-Research Cooperation Fund(SAST 2020-019).
Relative navigation is crucial for spacecraft noncooperative rendezvous,and angles-only navigation using visible and infrared cameras provides a feasible solution.Herein,an angles-only navigation algorithm with multis...
关键词：angles-only navigation feasibility analysis multisensor data fusion spacecraft noncooperative rendezvous 
End-to-end Mars entry,descent,and landing modeling and simulations for Tianwen-1 guidance,navigation,and control system被引量：3
《Astrodynamics》2022年第1期53-67,共15页Chao Xu Xiangyu Huang Minwen Guo Maodeng Li Jinchang Hu Xiaolei Wang 
This work was supported by the National Natural Science Foundation of China(No.61803028)and Civil Aerospace Advance Research Project.
On May 15,2021,the Tianwen-1 lander successfully touched down on the surface of Mars.To ensure the success of the landing mission,an end-to-end Mars entry,descent,and landing(EDL)simulator is developed to assess the g...
关键词：Mars entry descent and landing(EDL) modeling and simulation Tianwen-1 lander guidance navigation and control(GNC) 
Integrated constellation design and deployment method for a regional augmented navigation satellite system using piggyback launches被引量：2
《Astrodynamics》2021年第1期49-60,共12页Shuai Guo Wanmeng Zhou Jin Zhang Fuyu Sun Dateng Yu 
This work was partially supported by the National Natural Science Foundation of China(No.11572345);the Science Project of the National University of Defense Technology(Nos.ZK17-03-21 and ZK18-03-07).
The method proposed in this paper is adopted to solve problem B of the 9th China Trajectory Optimization Competition(CTOC).An accurate and economical constellation design strategy for regional augmented navigation sat...
关键词：constellation design regional navigation augmentation piggyback launches trajectory optimization 
Ground-based low altitude hovering technique of Hayabusa2被引量：1
《Astrodynamics》2020年第4期331-347,共17页Yuya Mimasu Kent Yoshikawa Go Ono Naoko Ogawa Fuyuto Terui Yuto Takei Takanao Saiki Yuichi Tsuda 
The asteroid explorer Hayabusa2 carries multiple rovers and separates them to land on an asteroid surface.One of these rovers,called MASCOT,was developed under the international cooperation between the Deutsches Zentr...
关键词：Hayabusa2 MASCOT low altitude hovering guidance navigation and control(GNC) 
Hayabusa2’s station-keeping operation in the proximity of the asteroid Ryugu被引量：1
《Astrodynamics》2020年第4期349-375,共27页Yuto Takei Takanao Saiki Yukio Yamamoto Yuya Mimasu Hiroshi Takeuchi Hitoshi Ikeda Naoko Ogawa Fuyuto Terui Go Ono Kent Yoshikawa Tadateru Takahashi Hirotaka Sawada Chikako Hirose Shota Kikuchi Atsushi Fuji Takahiro Iwata Satoru Nakazawa Masahiko Hayakawa Ryudo Tsukizaki Satoshi Tanaka Masanori Matsushita Osamu Mori Daiki Koda Takanobu Shimada Masanobu Ozaki Masanao Abe Satoshi Hosoda Tatsuaki Okada Hajime Yano Takaaki Kato Seiji Yasuda Kota Matsushima Tetsuya Masuda Makoto Yoshikawa Yuichi Tsuda 
The Japanese interplanetary probe Hayabusa2 was launched on December 3,2014 and the probe arrived at the vicinity of asteroid 162173 Ryugu on June 27,2018.During its 1.4 years of asteroid proximity phase,the probe suc...
关键词：small body mission station-keeping guidance navigation and control(GNC) optical and radiometric navigation 
Guidance, navigation, and control of Hayabusa2 touchdown operations被引量：1
《Astrodynamics》2020年第4期393-409,共17页Fuyuto Terui Naoko Ogawa Go Ono Seiji Yasuda Tetsuya Masuda Kota Matsushima Takanao Saiki Yuichi Tsuda 
Hayabusa2 is a Japanese sample return mission from the asteroid Ryugu.The Hayabusa2 spacecraft was launched on 3 December 2014 and arrived at Ryugu on 27 June 2018.It stayed there until December 2019 for in situ obser...
关键词：small body exploration touchdown ASTRODYNAMICS GUIDANCE NAVIGATION CONTROL 
Design and flight results of GNC systems in Hayabusa2 descent operations
《Astrodynamics》2020年第2期105-117,共13页Go Ono Fuyuto Terui Naoko Ogawa Yuya Mimasu Kent Yoshikawa Yuto Takei Takanao Saiki Yuichi Tsuda 
Hayabusa2 is a Japanese sample return mission from the near-Earth asteroid Ryugu.The Hayabusa2 spacecraft was launched on December 3,2014,and reached the asteroid on June 27,2018.It remained there until November 13,20...
关键词：small body exploration ASTRODYNAMICS GUIDANCE NAVIGATION control 
A symplectic moving horizon estimation algorithm with its application to the Earth-Moon L2 libration point navigation被引量：1
《Astrodynamics》2019年第2期137-153,共17页Xinwei Wang Haijun Peng 
The authors are grateful for the nancial support of the National Natural Science Foundation of China(Grant No.11772074).
Accurate state estimations are perquisites of autonomous navigation and orbit maintenance missions.The extended Kalman lter(EKF)and the unscented Kalman lter(UKF),are the most commonly used method.However,the EKF resu...
关键词：moving horizon estimation symplectic method quasilinearization variational principle L2 libration point NAVIGATION 
Overview of China’s 2020 Mars mission design and navigation被引量：19
《Astrodynamics》2018年第1期1-11,共11页Xiuqiang Jiang Bin Yang Shuang Li 
the National Natural Science Foundation of China(Grant No.11672126);Innovation Funded Project of Shanghai Aerospace Science and Technology(Grant No.SAST2015036);the Opening Grant from the Key Laboratory of Space Utilization,Chinese Academy of Sciences(LSU-2016-07-01);Funding of Jiangsu Innovation Program for Graduate Education(Grant No.KYZZ160170);the Fundamental Research Funds for the Central Universities;Funding for Outstanding Doctoral Dissertation in NUAA(Grant No.BCXJ16-10);The authors fully appreciate their financial supports.
Scheduled for an Earth-to-Mars launch opportunity in 2020,the China’s Mars probe will arrive on Mars in 2021 with the primary objective of injecting an orbiter and placing a lander and a rover on the surface of the R...
关键词：China’s Mars exploration mission orbiting landing and roaming orbit design navigation scheme 
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