Evaluation program was performed to apply digital techniques to stabilization and control problem; selection of mathematical techniques for system analysis and development of fabrication methods for hardware implementation; discrete state model of spacecraft reaction wheel and jet attitude control system was developed and computer simulations were performed; electronic control unit was constructed with semiconductor integrated microelectronics, and tested on air bearing simulator; mathematical model of system is presented and experimental performance compared with computer simulation.
Spacecraft digital controller
SAE-NASA Aerospace Vehicle Flight Control Conference -- Proc
SAE-NASA -- Proceedings of the Aerospace Vehicle Flight Control Conference ; 1965 Control
1965
7 pages
Aufsatz (Konferenz)
Englisch
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A spacecraft digital controller.
NTRS | 1965
|A Spacecraft Digital Controller
SAE Technical Papers | 1965
|