DocumentCode
3421991
Title
Trajectory generation for a UAV in urban terrain, using nonlinear MPC
Author
Singh, Leena ; Fuller, James
Author_Institution
United Technol. Res. Center, East Hartford, CT, USA
Volume
3
fYear
2001
fDate
2001
Firstpage
2301
Abstract
This paper describes a receding-horizon optimal control scheme for autonomous trajectory generation and flight control of an unmanned air vehicle in urban terrain. In such environments, the mission objective or terrain may be dynamic, and the vehicle may change dynamics mid-flight due to sensor or actuator failure; thus off-line pre-planned flight trajectories axe limiting and insufficient. This technology is aimed at supporting guidance and control for future missions that will require vehicles with increased autonomy in dangerous situations and with tight maneuvering and operational capability e.g., missions in urban environments. A Model Predictive Control (MPC) scheme is described here that navigates a vehicle with nonlinear dynamics through a vector of known way-points to a goal, and manages constraints. In this MPC-based approach to trajectory planning with constraints, a feedforward nominal trajectory is used to convert the nonconvex, nonlinear optimal control problem into a time-varying linear, convex optimization or quadratic programming problem. The nonconvex, admissible path space is converted to a sequence of overlapping, convex spaces. The feedforward control that produces the nominal trajectory is found from the vehicle´s differentially flat outputs. MPC is used to determine the optimal perturbations to the nominal control that will suitably navigate the vehicle through a constrained input/output space while minimizing actuation effort. Simulation results with a non-real-time, online MPC controller for a UAV in a planar urban terrain are included to support the proposed approach
Keywords
convex programming; linear systems; optimal control; predictive control; quadratic programming; time-varying systems; UAV; actuator failure; admissible path space; autonomous trajectory generation; constrained input/output space; convex optimization; feedforward nominal trajectory; flight control; flight trajectories; nonlinear model predictive control; operational capability; quadratic programming; receding-horizon optimal control; sensor failure; time-varying linear system; trajectory generation; unmanned air vehicle; urban terrain; Actuators; Aerospace control; Navigation; Optimal control; Predictive control; Predictive models; Remotely operated vehicles; Trajectory; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
Conference_Location
Arlington, VA
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.946095
Filename
946095
Link To Document