Control system is shown to be sized, in terms of required impulse capacity, by long term effects of gravity gradient and aerodynamic disturbances; reaction control propellant required to counteract disturbances is minimized by selection of attitude orientations which reduce external torques and by using momentum storage devices to counteract cyclic disturbances; examples of experimental mechanization with space station control system are described including earth surface tracking device, horizon spectrometry experiment and astronomical telescope.
Flight control for manned orbital space station
SAE-NASA -- Proc
Proceedings of the SAE-NASA -- Aerospace Vehicle Flight Control Conference ; 1965 Control
1965
32 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Flight Control for a Manned Orbital Space Station
SAE Technical Papers | 1965
|Flight control for a manned orbital space station.
NTRS | 1965
|A MULTIPURPOSE, MANNED, ORBITAL SPACE STATION
AIAA | 1963
|A MULTIPURPOSE, MANNED, ORBITAL SPACE STATION
NTRS | 1963
|