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The latter is tracked with a fast quadrant detector for precise attitude sensing and clock synchronization while the former passes a binary liquid-crystal-based half-wave plate switch (LC-HWP).
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As described in Part 1, current conventional reactive attitude sensing systems lack the necessary response times for attitude control in high turbulence environments.
Star sensor is one of the precise attitude determination sensors.
OGS and CubeSat point beacon lasers at each other for precise attitude control.
To achieve precise attitude stabilization, these small satellites should estimate their attitude rate under the strict constraints of mass, space, and cost.
Hence, the satellites can achieve precise attitude control under low power, space, and mass constraints using this proposed method.
Simulation results show that precise attitude control is accomplished based on the proposed method.
Simulation results for the spacecraft model show precise attitude control and vibration suppression.
These concepts require propulsion systems for precise attitude and orbit control manoeuvrability.
Moreover, each Swarm satellite carries three star trackers allowing a precise attitude reconstruction for all latitudes and local times.
Simulation results for the spacecraft model show that the precise attitudes control and vibration suppression are successfully achieved.
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