TY - GEN
T1 - Integrated optimal formation control of multiple unmanned aerial vehicles
AU - Wang, Jianan
AU - Xin, Ming
PY - 2012
Y1 - 2012
N2 - This paper investigates the formation control of multiple Unmanned Aerial Vehicles (UAVs), particularly unmanned aircraft, in an obstacle-laden environment. The main contribution of the paper is to integrate the formation control, trajectory tracking, and obstacle/collision avoidance into one unified optimal control framework. The non-quadratic avoidance cost is innovatively constructed via an inverse optimal control approach, which leads to an analytical, distributed, and optimal formation control law. The stability and optimality of the closed-loop system are proved. In addition, the proposed optimal control law is only dependent on the information from the local neighbors, rather than all UAVs' information. Simulation of multiple UAVs' formation flying demonstrates the effectiveness of the integrated optimal control design with desired behaviors including formation flying, trajectory tracking, and obstacle/collision avoidance.
AB - This paper investigates the formation control of multiple Unmanned Aerial Vehicles (UAVs), particularly unmanned aircraft, in an obstacle-laden environment. The main contribution of the paper is to integrate the formation control, trajectory tracking, and obstacle/collision avoidance into one unified optimal control framework. The non-quadratic avoidance cost is innovatively constructed via an inverse optimal control approach, which leads to an analytical, distributed, and optimal formation control law. The stability and optimality of the closed-loop system are proved. In addition, the proposed optimal control law is only dependent on the information from the local neighbors, rather than all UAVs' information. Simulation of multiple UAVs' formation flying demonstrates the effectiveness of the integrated optimal control design with desired behaviors including formation flying, trajectory tracking, and obstacle/collision avoidance.
UR - https://www.scopus.com/pages/publications/85087247094
U2 - 10.2514/6.2012-4459
DO - 10.2514/6.2012-4459
M3 - Conference contribution
AN - SCOPUS:85087247094
SN - 9781600869389
T3 - AIAA Guidance, Navigation, and Control Conference 2012
BT - AIAA Guidance, Navigation, and Control Conference 2012
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA Guidance, Navigation, and Control Conference 2012
Y2 - 13 August 2012 through 16 August 2012
ER -