Satellite pitch and roll attitude maneuvers through very short tethers

Acta Astronautica

Volumn 44, Issue 5-6, 1999, Pages 257-265

  Kumar, K D ^a   Kumar, Krishna ^a  

^a INDIAN INSTITUTE OF TECHNOLOGY KANPUR   (India)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION; FLIGHT DYNAMICS; LAGRANGE MULTIPLIERS; SPACE FLIGHT; TETHERLINES;

AUXILIARY MASS; OPEN LOOP TETHER LENGTH CONTROL LAWS; ROLL ATTITUDE MANEUVERS; SATELLITE PITCH; TETHERED SATELLITE SYSTEM;

SATELLITES;

EID: 0033099355     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(99)00019-3     Document Type: Article

References (21)

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