2025 IEEE International Conference on Advanced Robotics (ICAR)(2025)
CONICET - Universidad de San Andrés
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摘要
This work addresses the control problem of a foldable quadrotor whose in-flight arm reconfiguration changes its moment of inertia. A Linear Parameter Varying (LPV) controller is first designed to maintain consistent performance across configurations, but its computational cost limits its use on low-cost autopilots. Based on frequency domain analysis, we approximate the LPV with a low-order controller, akin to an adaptive PID, achieving similar response at lower complexity. Simulations and experimental tests on a Cortex M3-based platform, using both fixed-point and doubled-precision implementations, show similar behavior. The approach approximates LPV-like performance with PID-level efficiency, enabling real-time deployment on resource-constrained UAVs.
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关键词
Linear Parameter Varying,Control Problem,Moment Of Inertia,Autopilot,Control Strategy,Center Of Mass,Optimal Control,Fixed Point,Frequency Response,Adaptive Control,Tracking Error,Inertial Measurement Unit,Implementation Of Control,Tracking Accuracy,Sliding Mode Control,Roll Angle,Clock Cycles,Closed-loop Response,Roll Axis,Pitch Axis