TY - GEN
T1 - Integrating task assignment and guidance via motion planning for unmanned aerial vehicles
AU - Cons, Matthew S.
AU - Shima, Tal
AU - Domshlak, Carmel
PY - 2011
Y1 - 2011
N2 - The process of integrating task and motion planning for unmanned aerial vehicles is examined. Here, an unmanned aerial vehicle is modeled as a Dubins vehicle: a vehicle with a minimum turn radius and the inability to go backward. Given a starting position and orientation for a Dubins vehicle and a set of stationary targets, the main problem is to determine the shortest flyable path that visits each target. This problem is called the Dubins traveling salesman problem, an extension of the well-known traveling salesman problem. A number of algorithms with different approaches, including a hierarchical approach, a generalized traveling salesman problem reformulation approach, and a search with an upper bound Dubins cost approach, is developed and contrasted. Monte Carlo simulations were performed for a range of vehicle turn radii. Simulations results show that integrating two plausible kinematic satisfying paths as an upper bound to determine the cost-so-far into a search algorithm generally improves performance in terms of the shortest path cost and search complexity. Furthermore, when a suitable trajectory for traversing an ordered set of targets has been found, the applicability of using proportional navigation guidance is examined. It is shown that using a simple proportional navigation guidance law, stationary targets located within the vehicle's turn circle are unreachable. To address this issue, way-points are generated that will allow the vehicle to reach these hard targets with minimum distance. The waypoints are generated by solving a relaxed version of the point to point Dubins problem. In addition, it is shown that any trajectory composed of point to point Dubins paths can be navigated using proportional navigation with a minimum number of waypoints, regardless of the target positions.
AB - The process of integrating task and motion planning for unmanned aerial vehicles is examined. Here, an unmanned aerial vehicle is modeled as a Dubins vehicle: a vehicle with a minimum turn radius and the inability to go backward. Given a starting position and orientation for a Dubins vehicle and a set of stationary targets, the main problem is to determine the shortest flyable path that visits each target. This problem is called the Dubins traveling salesman problem, an extension of the well-known traveling salesman problem. A number of algorithms with different approaches, including a hierarchical approach, a generalized traveling salesman problem reformulation approach, and a search with an upper bound Dubins cost approach, is developed and contrasted. Monte Carlo simulations were performed for a range of vehicle turn radii. Simulations results show that integrating two plausible kinematic satisfying paths as an upper bound to determine the cost-so-far into a search algorithm generally improves performance in terms of the shortest path cost and search complexity. Furthermore, when a suitable trajectory for traversing an ordered set of targets has been found, the applicability of using proportional navigation guidance is examined. It is shown that using a simple proportional navigation guidance law, stationary targets located within the vehicle's turn circle are unreachable. To address this issue, way-points are generated that will allow the vehicle to reach these hard targets with minimum distance. The waypoints are generated by solving a relaxed version of the point to point Dubins problem. In addition, it is shown that any trajectory composed of point to point Dubins paths can be navigated using proportional navigation with a minimum number of waypoints, regardless of the target positions.
UR - http://www.scopus.com/inward/record.url?scp=85088339082&partnerID=8YFLogxK
U2 - https://doi.org/10.2514/6.2011-6387
DO - https://doi.org/10.2514/6.2011-6387
M3 - منشور من مؤتمر
SN - 9781600869525
T3 - AIAA Guidance, Navigation, and Control Conference 2011
BT - AIAA Guidance, Navigation, and Control Conference 2011
T2 - AIAA Guidance, Navigation and Control Conference 2011
Y2 - 8 August 2011 through 11 August 2011
ER -