DocumentCode
1935274
Title
Optimal merging of multiple aircrafts to waypoints via controlled time of arrival windows
Author
Poolla, Chaitanya ; Ishihara, A.K.
Author_Institution
Electr. & Comput. Eng., Carnegie Mellon SV, Moffett Field, CA, USA
fYear
2013
fDate
2-9 March 2013
Firstpage
1
Lastpage
6
Abstract
This paper presents an algorithm that computes the optimal arrival times and velocities required for maximizing worst case mutual separation in a multiple aircraft optimal merging scenario. The approach leverages the Pontryagin Maximum Principle (PMP) to rapidly generate locally optimal trajectories per aircraft and an outer-loop Particle Swarm Optimization (PSO) scheme to search for globally optimal merging dynamics. The subset of feasible Controlled Time of Arrival (CTA) and velocity windows is estimated based on an asymptotic approximation of the locally optimal trajectory generated by the PMP. The Particle Swarm Optimization (PSO) scheme maximizes the minimum separation between all aircrafts over all instances of the trajectory. The cost functional has been chosen to minimize load factor (enhance comfort) and maximize worst case mutual separation (improve safety). Simulations based on a simplified lateral aircraft model subject to bounded control inputs are provided to illustrate the concept.
Keywords
aircraft control; optimal control; particle swarm optimisation; CTA; PMP; PSO scheme; asymptotic approximation; controlled time of arrival windows; globally optimal merging dynamics; locally optimal trajectories per aircraft; locally optimal trajectory; multiple aircraft optimal merging scenario; outer-loop PSO scheme; outer-loop particle swarm optimization scheme; particle swarm optimization scheme; pontryagin maximum principle; simplified lateral aircraft model; Aircraft; Merging; ATC automation; CTAs; NextGen FMS; Optimal Lateral Trajectory; Separation assurance;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2013 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4673-1812-9
Type
conf
DOI
10.1109/AERO.2013.6496934
Filename
6496934
Link To Document