Design characteristics of thruster configurations for spacecraft attitude control systems investigated. A standard six engine approach is developed and used as the basis for comparison of different thruster configurations. These methods include cases of both skewed and non-skewed configurations. Simulation results are used as a basis for comparison, critical thruster design factors being given based on an analysis of the data.
New thruster configurations for spacecraft attitude control systems
Engineering in a changing economy ; 1976 ; Clemson, SC
1976-01-01
Miscellaneous
No indication
English
Disturbance Accommodating Spacecraft Attitude Control Using Thruster
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