Title :
Multi-rotor robust trajectory tracking
Author :
Gil-Martinez, M. ; Rico-Azagra, J.
Author_Institution :
Electr. Eng. Dept., Univ. of La Rioja, Logrono, Spain
Abstract :
This paper develops a position control strategy of a multi-rotor system, which moves from an X-Y way-point to another at constant maximum-achievable velocity, and follows rectilinear trajectories between way-points with slight deviations during transients. In achieving this, 2D-spatial displacement breaks down in time domain ramp tracking on each axis through a trajectory generation block. Then, both axis set-points are driven to model matching feedback control structures that compute the roll and pitch angles commands. Main feedback control challenges are addressing a large model uncertainty identified for the inner attitude-controlled multi-copter, and a small control-bandwidth due to angle-saturation and due to processor sample-time. In this framework the Quantitative Feedback Theory has succeed in the robust design of feedback and feed-forward control elements. Some final tests demonstrate the expected spatial and time domain performances.
Keywords :
aircraft control; attitude control; autonomous aerial vehicles; feedback; feedforward; helicopters; position control; robust control; trajectory control; uncertain systems; 2D-spatial displacement; UAV; X-Y way-point; angle-saturation; axis set-points; constant maximum-achievable velocity; control-bandwidth; inner attitude-controlled multicopter; model matching feedback control structures; multirotor robust trajectory tracking; pitch angle command; position control strategy; processor sample time; quantitative feedback theory; rectilinear trajectories; robust feed-forward control element design; robust feedback control element design; roll angle command; spatial domain performances; time domain performances; time domain ramp tracking; trajectory generation block; transients; unmanned aerial vehicles; Attitude control; Feedback control; Position control; Robustness; Steady-state; Trajectory; Uncertainty; 2D Position Control; Model Matching; Quantitative Feedback Theory (QFT); Tracking Error; Trajectory Generation; UAVs;
Conference_Titel :
Control and Automation (MED), 2015 23th Mediterranean Conference on
Conference_Location :
Torremolinos
DOI :
10.1109/MED.2015.7158854