A Single CCD Algorithm to Determine the Position and Attitude during Rolling Phase of Rendezvous and Docking

Article Preview

Abstract:

Propose a new algorithm that use Euler angles to calculate directly large relative position and attitude of rendezvous and docking. By analyzing the feasibility of using Euler angles to solve instead of using quaternion and deriving the relations between the coordinates of the identification-points and the coordinates of point-images, a group of non-linear equations including relative position and attitude is established. It is proved that three non-collinear points are sufficient and required to determine the position and attitude uniquely. The whole deriving process does not mention any assumption and simplification in theory. Simulations indicate that the algorithm is high-accurate, unique-solution and wide application scope.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

813-818

Citation:

Online since:

July 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Yang Jin, Jiang Guohua, Chao Jian-gang. "A cross done image-based manual control rendezvous and docking method",Journal of astronautics, 2010.

Google Scholar

[2] N. K. Philip, M. R. Ananthasayanam. "Relative position and attitude estimation and control schemes for the final phase of an autonomous docking mission of spacecraft",Acta Astronautica, 2003, pp.511-522.

DOI: 10.1016/s0094-5765(02)00125-x

Google Scholar

[3] Zhao Tianyun, Guo Lei, Zhang Lichuan. "A New Algorithm of Spatial Positioning Based on Mono-Vision", Journal of northwestern polytechnical university, 2009.

Google Scholar

[4] R. Mukundan. "A quaternion solution to the pose determination problem for rendezvous and docking simulations",Mathematics and computers in simulation, 1995, pp.143-153.

DOI: 10.1016/0378-4754(95)00028-v

Google Scholar

[5] Zhao Yuhua, Yuan Feng, Ding Zhenliang. "Posture measurement of aircraft based on cooperation target and its error compensation", Electric machines and control, 2010.

Google Scholar

[6] Zhang Shijie, Cao Xibin, Chen Xueqin. "Closed form method for relative pose parameters of spacecraft based on optical measurement", Acta Aeronautica et Astronautica Sinica, 2005, pp.216-218.

Google Scholar

[7] Zhang Shijie, Liu Fenghu, Cao Xibin. "Monocular Vision-based Two-stage Iterative Algorithm for Relative Position and Attitude Estimation of Docking Spacecraft", Chinese journal of aeronautics, 2010.

DOI: 10.1016/s1000-9361(09)60206-5

Google Scholar

[8] Zhang Shijie, Cao Xibin, Chen Xueqin. "Closed-Form Method for Relative Pose Parameters of Spacecraft Based on Optical Measurement", Acta Aeronautica et Astronautica Sinica, (2005)

Google Scholar

[9] Fei Weichun. "Estimation method of relative position and attitude in spacecraft rendezvous and docking",Systems Engineering and Electronics, 2004, pp.1282-1286.

Google Scholar

[10] Zhu Renzhang, Lin Yan, Zhang Lei. "New algorithm of solving for range during final approach of spacecraft rendezvous",Journal of Beijing University of Aeronautics and Astronautics, 2006, pp.764-768.

Google Scholar