Add to ORKGThe article of record as published may be found at http://dx.doi.org/10.1177/0954410018787866Spacecr...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The use of inertia wheels to control the attitude of a satellite has currently aroused much interest...
Suboptimal compensation of gyroscopic coupling for inertia-wheel attitude control by mathematical te...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
This paper examines the usefulness of variable inertia reaction wheels (VIRWs) for spacecraft attitu...
Simulation tests of attitude control system that uses star trackers and inertia wheel
This book consists of two main parts main goal of the first part is to collect and develop new atti...
The article of record as published may be found at http://doi.org/10.2514/1.G002460This paper propos...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140657/1/1.G001446.pd
A4attitude control systemn coný5-Stz~na Of mnotor-driven inriaw..ýecls in. uz:;nw~hat. orriignsseeco...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The article of record as published may be found at http://dx.doi.org/10.1177/0954410018787866Spacecr...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The use of inertia wheels to control the attitude of a satellite has currently aroused much interest...
Suboptimal compensation of gyroscopic coupling for inertia-wheel attitude control by mathematical te...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
Automatic attitude control system test for satellite using inertia wheels mounted on air bearing
This paper examines the usefulness of variable inertia reaction wheels (VIRWs) for spacecraft attitu...
Simulation tests of attitude control system that uses star trackers and inertia wheel
This book consists of two main parts main goal of the first part is to collect and develop new atti...
The article of record as published may be found at http://doi.org/10.2514/1.G002460This paper propos...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140657/1/1.G001446.pd
A4attitude control systemn coný5-Stz~na Of mnotor-driven inriaw..ýecls in. uz:;nw~hat. orriignsseeco...
Mathematical model for determining minimax attitude control of aeroballistic launch vehicles - stabi...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The article of record as published may be found at http://dx.doi.org/10.1177/0954410018787866Spacecr...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The use of inertia wheels to control the attitude of a satellite has currently aroused much interest...