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ATTITUDE
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keywords:(SATELLITE ATTITUDE CONTROL)
Attitude Determination and Control Systems
OPTEC: A Cubesat for Solar Cell Calibration
Position Determination of a Stationary TV Communications Satellite with Horizon Sensors
Research on the Design of Adaptive Control Systems, Volume 2 Final Report
The Magnetic Torquing System Used on the Ariel 4 Spacecraft
Spacecraft Gravitational Torques - NASA Space Vehicle Design Criteria (Guidance and Control)
Attitude Stability of a Class of Partially Flexible Spinning Satellites
Attitude Stabilization of a Rigid Spacecraft Using Two Momentum Wheel Actuators
Space Technology 5 - A Successful Micro-Satellite Constellation Mission
Satellite Yaw Attitude Measurement Methods and Systems Study
Attitude Analysis of the Earth Radiation Budget Satellite (ERBS) Yaw Turn Anomaly
Attitude Motion of a Non-Attitude-Controlled Cylindrical Satellite
Coupled Orbit and Attitude Motion of Spacecraft
Satellite Yaw Sensor Study Program Final Report
TRMM On-Orbit Performance Re-Accessed After Control Change
An Automatic Attitude Control System for a Spinning Satellite - a Theoretical Assessment
Applications Technology Satellite Ats-6 in Orbit Checkout Report
Attitude Perturbations and Magnetic Control of a Spin-Stabilized Satellite, Part II
Analysis and Design of Space Vehicle Flight Control Systems. Volume XII - Attitude Control in Space
Satellite Orbit and Attitude Theory and Its Use with Skynet 2
Satellite Orbit and Attitude Theory and Its Use with Skynet 2
Spacecraft Control Section for the Improved Small Astronomy Satellite (Sas)
Attitude Stabilization of a Rigid Spacecraft Using Gas Jet Actuators Operating in a Failure Mode
Shaded Sun Sensor Modeling for Spacecraft Acquisition Performance Analysis
A Study of a Gravity-Gradient-Stabilized Nimbus Spacecraft Final Study Report, Jul. - Dec. 1965
Evaluation of the Communications Technology Satellite Attitude Acquisition Algorithms and Procedures
An Active and/or Passive Spacecraft Attitude Control
Microwave Anisotropy Probe (MAP): Guidance, Navigation, and Control Hardware Suite
Satellite Attitude Control System, Using Integrating Gyros as Torquers
AE-5 End of Mission Tests Report
Estimation of the Local Attitude of Orbiting Spacecraft
Techniques for Earth-Pointing Attitude Control of a Spacecraft
Techniques for Earth-Pointing Attitude Control of a Spacecraft
Control and Stabilisation of Spacecraft. Volume 1 - Introduction and Seminars
Attitude Estimation for Low-Cost Spacecraft Equipped with GPS
A Test of the Effect of Satellite Spin on Two- Way Doppler Range-Rate Measurements
On the Application of Electric Propulsion to Satellite Orbit Adjustment and Station Keeping
Analytical Methods for Resistance Jet Design Supplementary Report No. 1