Add to ORKGThe design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
The mission requirements for some satellites require that they spin continuously and at the same tim...
A design and performance evaluation is presented for the LANDSAT D attitude control system (ACS). Co...
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
A satellite precision attitude control system was designed, based on the use of STARS as the princip...
The performance capability of each of two precision attitude determination systems (PADS), one using...
Space vehicle attitude control systems - manned space station, satellite in elliptic orbit, and sola...
Spacecraft attitude control with strapdown inertial reference system and onboard digital compute
Gyroscope system for inertial experiment pointing and attitude control of manned spacecraf
A conceptual design for a double-gimbal reaction-wheel energy-wheel device which has three-axis atti...
Development of the Precision Attitude Determination System (PADS) focused chiefly on the two-axis gi...
Attitude requirements of a satellite are determined by its mission: telecommunications, optical imag...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
Suboptimal systems synthesis using motor-driven inertia wheels for attitude contro
Attitude control of a satellite is required for the pointing of communications antennas and other in...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
The mission requirements for some satellites require that they spin continuously and at the same tim...
A design and performance evaluation is presented for the LANDSAT D attitude control system (ACS). Co...
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
A satellite precision attitude control system was designed, based on the use of STARS as the princip...
The performance capability of each of two precision attitude determination systems (PADS), one using...
Space vehicle attitude control systems - manned space station, satellite in elliptic orbit, and sola...
Spacecraft attitude control with strapdown inertial reference system and onboard digital compute
Gyroscope system for inertial experiment pointing and attitude control of manned spacecraf
A conceptual design for a double-gimbal reaction-wheel energy-wheel device which has three-axis atti...
Development of the Precision Attitude Determination System (PADS) focused chiefly on the two-axis gi...
Attitude requirements of a satellite are determined by its mission: telecommunications, optical imag...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
Suboptimal systems synthesis using motor-driven inertia wheels for attitude contro
Attitude control of a satellite is required for the pointing of communications antennas and other in...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
The mission requirements for some satellites require that they spin continuously and at the same tim...
A design and performance evaluation is presented for the LANDSAT D attitude control system (ACS). Co...