Differential Flatness-based Fast Trajectory Planning for Fixed-wing Unmanned Aerial Vehicles

Due to the strong nonlinearity and nonholonomic dynamics, despite that various general trajectory optimization methods have been presented, few of them can guarantee efficient compu-tation and physical feasibility for relatively complicated fixed-wing UAV dynamics. Aiming at this issue, this paper investigates a differential flatness-based trajectory optimization method for fixed-wing UAVs (DFTO-FW), which transcribes the trajectory optimization into a lightweight, unconstrained, gradient-analytical optimization with linear time complexity in each itera-tion to achieve fast trajectory generation. Through differential flat characteristics analysis and polynomial parameterization, the customized trajectory representation is presented, which implies the equality constraints to avoid the heavy computational burdens of solving complex dynamics. Through the design of integral performance costs and deduction of analytical gradients, the original trajectory optimization is transcribed into an uncon-strained, gradient-analytical optimization with linear time com-plexity to further improve efficiency. The simulation experi-ments illustrate the superior efficiency of the DFTO-FW, which takes sub-second CPU time against other competitors by orders of magnitude to generate fixed-wing UAV trajectories in ran-domly generated obstacle environments.