Morphing Process Research of UAV with PID Controller
Jan 01, 2015 · Simulation Nonlinear simulation of the longitudinal model of morphing UAV run with PID controller, the initial condition include flight height 1000 m and flight speed 66 m/s. the following description is control strategy about morphing UAV. Wing shrinking time happen within 50s and 200s, and thrust force keep 150N before 50s.
DA: 15 PA: 30 MOZ Rank: 15