New approach to halo orbit determination and control

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 2, 1996, Pages 266-273

  Cielaszyk, David ^a,b,c   Wie, Bong ^a,b  

^a ARIZONA STATE UNIVERSITY   (United States)

^b Dept of Mech and Aerosp Eng ^*

^c Safety and Mission Assurance Manager Space Systems Loral   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL NONLINEARITIES; EQUATIONS OF MOTION; ITERATIVE METHODS; LINEAR CONTROL SYSTEMS; SPACECRAFT; TRAJECTORIES; VECTORS;

CIRCULAR RESTRICTED THREE BODY PROBLEM; DISTURBANCE ACCOMMODATING; FIRST ORDER REFERENCE TRAJECTORY; HALO ORBIT; LISSAJOUS TRAJECTORY;

ORBITS;

EID: 0030107875     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21614     Document Type: Article

References (14)

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13. Cielaszyk, D., "A New Approach to Halo Orbit Determination and Control," M.S. Thesis, Dept. of Mechanical and Aerospace Engineering, Arizona State Univ., Tempe, AZ, Dec. 1993.
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