Iterative method for vision-based relative pose parameters of RVD spacecrafts

Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology

Volumn 37, Issue 8, 2005, Pages 1123-1126

  Cao, Xi Bin ^a   Zhang, Shi Jie ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Levenberg Marquardt algorithm; Monocular vision; Relative pose; Spacecraft

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; COMPUTER VISION; DOCKING; ITERATIVE METHODS;

LEVENBERG MARQUARDT ALGORITHM; MONOCULAR VISION; RELATIVE POSE;

SPACECRAFT;

EID: 25144521028     PISSN: 03676234     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. HO C J, MCDLAMROCH N H. Automatic spacecraft docking using computer vision-based guidance and control techniques [J]. Journal of Guidance, Control, and Dynamics, 1993, 16(2): 281-288.
2. PHILIP N K, ANANTHASAYANAM M R. Relative position and attitude estimation and control schemes for the final phase of an autonomous docing mission of spacecraft [J]. Acta Astronautica, 2003, 52: 511-522.
3. MUKUNDAN R, RAMAKRISHNAN K R. A quaternion solution to the pose determination problem for rendezvous and docking simulations [J]. Mathematics and Computers in Simulation, 1995, 39: 143-153.