论文信息 - A Velocity and Distance Control System Synthesis Using Dynamic Inversion with PI Control

A Velocity and Distance Control System Synthesis Using Dynamic Inversion with PI Control

The purpose of this paper is to introduce a velocity and distance control system for leader-following UAVs. In our previous paper, we already proposed a velocity and distance control system, but the system has a problem of ``offsets'' due to aerodynamic errors and/or leader trajectories. So in this paper, in order to eliminate the offset, a new approach of the velocity and distance control design is introduced. Simulation results show that the proposed velocity and distance control system provides a good performance and there are no offsets.

Keisuke Enomoto | Takeshi Yamasaki | Hiroyuki Takano | Yoriaki Baba

[1] Keisuke Enomoto,et al. Velocity Control System Design for Leader-Following UAV Using Dynamic Inversion , 2009 .

[2] Robert F. Stengel,et al. Flight Control Design using Nonlinear Inverse Dynamics , 1986, 1986 American Control Conference.

[3] Yoshimasa Ochi,et al. Flight Control for Automatic Aerial Refueling via PNG and LOS Angle Control , 2005 .

[4] H. Takano,et al. Flight Trajectory Tracking System Applied to Inverse Control for Aerobatic Maneuvers , 2002 .

[5] Keisuke Enomoto,et al. Automatic Control for Chase Aircraft , 2006 .

[6] K. Enomoto,et al. Robust trajectory-tracking method for UAV guidance using proportional navigation , 2007, 2007 International Conference on Control, Automation and Systems.

[7] Keisuke Enomoto,et al. Guidance and Control System Design for Chase UAV , 2008 .

[8] S. A. Snell. Preliminary assessment of the robustness of dynamic inversion based flight control laws , 1992 .