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What is Adaptive Control for Spacecraft Maneuvers about?

This paper presents an adaptive control methodology for spacecraft attitude tracking that accounts for actuator saturation constraints. The key aspects are: 1) When control saturation occurs, the reference trajectory is modified to approximate the original while remaining within saturation limits. This prevents parameter drift in the adaptive control from errors due to saturation. 2) Tracking error is defined between the plant and modified reference trajectory, avoiding error components from saturation.

Author

dursun_ufuk

Language

EN