Steady state off-on attitude control strategy for minimizing propellant consumption and thrust ignitions of satellite in presence of environmental disturbance torques
A minimum-fuel mode for steady-state attitude control of an earth-orbiting spacecraft
1970-06-01
Miscellaneous
No indication
English
A quasi-inertial attitude mode for orbiting spacecraft.
AIAA | 1972
|In-Flight Attitude Perturbation Estimation for Earth-Orbiting Spacecraft
Springer Verlag | 2009
|A quasi-inertial attitude mode for orbiting spacecraft.
NTRS | 1972
|In-Flight Attitude Perturbation Estimation for Earth-Orbiting Spacecraft
Online Contents | 2009
|In-Flight Attitude Perturbation Estimation for Earth-Orbiting Spacecraft
Springer Verlag | 2009
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