CORDIS Project
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This project focuses on developing innovative control algorithms for stabilizing the orientation of small spacecraft, particularly in cases of actuator failure. It aims to enhance reliability by addressing the challenges of nonholonomic systems and ensuring performance even with limited control options.
Space stakeholders manifest an increasing interest in small satellites dictated by reduced, global costs and “time to market”.
Since redundancy is kept to a minimum, achieving attitude stabilization in actuator failure mode with the remaining control torques can offer a fail-safe operation mode, improving the reliability of the attitude control system.
The, still open, underlying control problem is challenging, since the nonlinear underactuated system is nonholonomic, admitting only non-smooth s…
UNIVERSITA DEGLI STUDI DI ROMA LA SAPIENZA
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