Multi-Objective UAS Flight Management in Time Constrained Low Altitude Local Environments

No Altmetrics are currently available for this publication.

Narayan, P. P., Campbell, D. A. and Walker, R. A. (2008) Multi-Objective UAS Flight Management in Time Constrained Low Altitude Local Environments. In: 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 7-10 January, 2008. Reno, Nevada, USA: American Institute of Aeronautics and Astronautics, pp. 1-14 Available from: http://eprints.uwe.ac.uk/18332

[img]
Preview
PDF
AIAA Conference Paper Jan 2008 Reno - Pritesh Narayan - eprints.pdf - Submitted Version

Download (295kB) | Preview
Publisher's URL: http://www.aiaa.org/

Abstract/Description

This paper presents a new framework for Multi-Objective Flight Management of Unmanned Aerial Systems (UAS), operating in partially known environments, where planning time constraints are present. During UAS operations, civilian UAS may have multiple objectives to meet including: platform safety; minimizing fuel, time, distance; and minimizing deviation from the current path. The planning layers within the framework use multi-objective optimization to converge to a solution which better reflects overall mission requirements. The solution must be generated within the available decision window, else the UAS must enter a safety state; this potentially limits mission efficiency. Local or short range planning at low altitudes requires the classification of terrain and infrastructure in proximity as potential obstacles. The potential increase in the number of obstacles present further reduces the decision window in comparison to high altitude flight. A novel Flight Management System (FMS) has been incorporated within the framework to moderate the time available to the environment abstraction, path and trajectory planning layers for more efficient use of the available decision window. Enabling the FMS during simulation increased the optimality of the output trajectory on systems with sufficient computational power to run the algorithm in real time. Conversely, the FMS found sub-optimal solutions for the system with insufficient computational capability once the objective utility threshold was decreased from 0.95 to 0.85. This allowed the UAS to continue operations without having to resort to entering a safe state.

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: UAS, UAV, trajectory generation, manoeuvre automata, multi, objective, real time, flight management
Faculty/Department: Faculty of Environment and Technology > Department of Engineering Design and Mathematics
Depositing User: Dr P. Narayan
Date Deposited: 16 Jan 2013 11:40
Last Modified: 17 Jun 2016 23:03
URI: http://eprints.uwe.ac.uk/id/eprint/18332

Statistics

Downloads
Activity Overview
122Downloads
274Hits
Origin of downloads

Additional statistics for this repository are available via IRStats2

Actions (login required)

View Item View Item