Control and flight performance of tethered satellite small expendable deployment system-II

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 5, 1996, Pages 1148-1156

  Lorenzini, E C ^a,d   Bortolami, S B ^a,c   Rupp, C C ^b   Angrilli, F ^c  

^a HARVARD SMITHSONIAN CENTER FOR ASTROPHYSICS   (United States)

^b NASA MARSHALL SPACE FLIGHT CENTER   (United States)

^c UNIVERSITY OF PADOVA   (Italy)

^d University of Padua ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL THEORY; FLIGHT DYNAMICS; LINEAR CONTROL SYSTEMS; LINEARIZATION; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; SPACE PROBES; TETHERLINES; TRAJECTORIES;

LIBRATION AMPLITUDE; ONBOARD COMPUTER; REFERENCE TRAJECTORY; SMALL EXPENDABLE DEPLOYMENT SYSTEM; TETHERED SATELLITE SYSTEM;

SATELLITES;

EID: 0030241321     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21757     Document Type: Article

References (19)

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