The attitude control module of the Spacecraft Control Toolbox provides the user with example attitude control systems. Designs include a complete sun-nadir pointing satellite attitude and momentum control system, a system for a maneuvering satellite using reaction wheels and a bias momentum satellite design.
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Key Features
The attitude control module provides the following point designs:
- Sun nadir pointing spacecraft using reaction wheels for pointing control and magnetic torquers for momentum control.
- Momentum bias geosynchronous spacecraft control system including both mission and transfer orbit.
- Spinning spacecraft with reaction wheel control.
- A double pivoted momentum wheel roll/yaw control system.
- An attitude maneuvering system.
- Magnetic control algorithms for instantaneous two-axis and average three axis control.
