On attitude maneuver of spinning tethered formation flying based on virtual structure method

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 4, Issue , 2005, Pages 2536-2552

  Nakaya, Koji ^a,c,d   Matunaga, Saburo ^b,d,e  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOKYO INSTITUTE OF TECHNOLOGY   (Japan)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^d AIAA   (United States)

^e Department of Mechanical and Aerospace Engineering ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEMS; FUEL CONSUMPTION; MATHEMATICAL MODELS; TETHERLINES;

ATTITUDE MANEUVERS; FLYING SYSTEM; SPINNING TETHERED FORMATION; VIRTUAL STRUCTURE METHOD;

MANEUVERABILITY;

EID: 29744435145     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6088     Document Type: Conference Paper

References (19)

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2. Nakaya, K., Iai, M., Mori, O. and Matunaga, S., "On Formation Deployment for Spinning Tethered Formation Flying and Experimental Demonstration," 18th International Symposium on Space Flight Dynamics, Munich, Germany, Oct.11-15, 2004
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