DocumentCode :
1339627
Title :
Near-Optimal Terrain Collision Avoidance Trajectories using Elevation Maps
Author :
Malaek, S.M. ; Abbasi, A.
Author_Institution :
Dept. of Aerosp. Eng., Sharif Univ. of Technol., Tehran, Iran
Volume :
47
Issue :
4
fYear :
2011
fDate :
10/1/2011 12:00:00 AM
Firstpage :
2490
Lastpage :
2501
Abstract :
The main attempt of this paper is to present a new methodology to model a generic low-level flight close to terrain, which guarantees terrain collision avoidance. Benefiting the advantages of high-speed computer technology, this method uses satellite elevation maps to generate so-called "quad-tree forms." The latter is then used to find the optimal trajectories for low-level flights. The novelty of this approach, entitled the "cost map," lies in the integration of aircraft dynamics into the segmented map. This procedure results in some near-optimal trajectories with respect to aircraft dynamics that could easily be used for minimization of flight path together with pilot effort. Different simulations show the method is applicable wherever there is no need for sharp changes in flight level. Nevertheless, the current method could be expanded to three-dimensional terrain avoidance/terrain following flights.
Keywords :
aircraft control; collision avoidance; control engineering computing; optimal control; position control; aircraft dynamics integration; generic low level flight; high speed computer technology; map elevation; near optimal terrain collision avoidance trajectory; near optimal trajectories; quad tree form; satellite elevation maps; terrain collision avoidance; Aerospace control; Collision avoidance; Cost function; Heuristic algorithms; Terrain mapping; Trajectory;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2011.6034646
Filename :
6034646
Link To Document :
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