A preliminary 6 DOF attitude and translation control system design for StarprobeThe extreme thermal environment near perihelion and the high-accuracy gravitational science experiments impose unique design requirements on various subsystems of Starprobe. This paper examines some of these requirements and their impact on the preliminary design of a six-degree-of-freedom attitude and translational control system. Attention is given to design considerations, the baseline attitude/translational control system, system modeling, and simulation studies.
Document ID
19820029606
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mak, P. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mettler, E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Vijayarahgavan, A. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)