Add to ORKGSingle axis simulator design for satellite control system testing and low torque measuremen
A design and performance evaluation is presented for the LANDSAT D attitude control system (ACS). Co...
Development and characteristics of simulation concept to analyze man, machine, and environment aspec...
Computer program documentation and user manual for steady state attitude control propulsion system -...
Analytic platform inertial navigation system using single axis reference and pendulous integrating g...
The kinematic parameters of position, velocity, and acceleration of a flight simulator may be calcul...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
Simulation tests of attitude control system that uses star trackers and inertia wheel
A compendium of techniques and basic information useful to the preliminary performance analysis of p...
A simulator is described, which was designed for testing and evaluating inertial measuring units, an...
In order to demonstrate the measurement of aerodynamic forces/moments, including the effects of exha...
The Earth's first artificial satellite, Sputnik 1, slowly tumbled in orbit. The first U.S. satellite...
The problem of applying modular attitude control to a rigid body - flexible suspension model of a fl...
In order to satisfy a growing demand for low cost attitude control systems for small spacecraft, dev...
All the available torque equilibrium attitudes (most were useless from the standpoint of lack of ele...
Applied Research Corporation (ARC) has developed an engineering model of a multi-star CCD-based trac...
A design and performance evaluation is presented for the LANDSAT D attitude control system (ACS). Co...
Development and characteristics of simulation concept to analyze man, machine, and environment aspec...
Computer program documentation and user manual for steady state attitude control propulsion system -...
Analytic platform inertial navigation system using single axis reference and pendulous integrating g...
The kinematic parameters of position, velocity, and acceleration of a flight simulator may be calcul...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
Simulation tests of attitude control system that uses star trackers and inertia wheel
A compendium of techniques and basic information useful to the preliminary performance analysis of p...
A simulator is described, which was designed for testing and evaluating inertial measuring units, an...
In order to demonstrate the measurement of aerodynamic forces/moments, including the effects of exha...
The Earth's first artificial satellite, Sputnik 1, slowly tumbled in orbit. The first U.S. satellite...
The problem of applying modular attitude control to a rigid body - flexible suspension model of a fl...
In order to satisfy a growing demand for low cost attitude control systems for small spacecraft, dev...
All the available torque equilibrium attitudes (most were useless from the standpoint of lack of ele...
Applied Research Corporation (ARC) has developed an engineering model of a multi-star CCD-based trac...
A design and performance evaluation is presented for the LANDSAT D attitude control system (ACS). Co...
Development and characteristics of simulation concept to analyze man, machine, and environment aspec...
Computer program documentation and user manual for steady state attitude control propulsion system -...