Efficient Reorientation Maneuvers for Spacecraft with Multiple Articulated PayloadsA final report is provided which describes the research program during the period 3 Mar. 1992 to 3 Jun. 1993. A summary of the technical research questions that were studied and of the main results that were obtained is given. The specific outcomes of the research program, including both educational impacts as well as research publications, are listed. The research is concerned with efficient reorientation maneuvers for spacecraft with multiple articulated payloads.
Document ID
19930020799
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Mcclamroch, N. Harris (Michigan Univ. Ann Arbor, MI, United States)
IDRelationTitle19930020801WorkAttitude stabilization of a rigid spacecraft using two momentum wheel actuators19930020802WorkNonlinear Attitude Control of Planar Structures in Space Using Only Internal Controls19930020803WorkAttitude stabilization of a rigid spacecraft using gas jet actuators operating in a failure mode19930020804WorkPlanar reorientation of a free-free beam in space using embedded electromechanical actuators19930020805WorkEfficient reorientation of a deformable body in space: A free-free beam example19930020806WorkSpace station attitude disturbance arising from internal motions19930020800WorkControl of nonlinear systems with applications to constrained robots and spacecraft attitude stabilization