DocumentCode
3551073
Title
Deciding to land a UAV safely in real time
Author
Sprinkle, Jonathan ; Eklund, J. Mikael ; Sastry, S. Shankar
Author_Institution
Dept. of Electr. Eng. & Comput. Sci., California Univ., Berkeley, CA, USA
fYear
2005
fDate
8-10 June 2005
Firstpage
3506
Abstract
The difficulty of autonomous free-flight of a fixed-wing UAV is trivial when compared to that of takeoff and landing. There is an even more marked difference when deciding whether or not a UAV can capture or recapture a certain trajectory, since the answer depends on the operating ranges of the aircraft. A common example of requiring this calculation, from a military perspective, is the determination of whether or not an aircraft can capture a landing trajectory (i.e., glideslope) from a certain initial state (velocity, position, etc.). As state dimensions increase, the time to calculate the decision grows exponentially. This paper describes how we can make this decision at flight time, and guarantee that the decision gives a safe answer before the state changes enough to invalidate the decision. We also describe how the computations should be formulated, and how the partitioning of the state-space can be done to reduce the computation time required. Flight testing was performed with our design, and results are given.
Keywords
aircraft; aircraft testing; mobile robots; remotely operated vehicles; autonomous free-flight; fixed-wing UAV; flight testing; landing trajectory; state dimensions; state-space partitioning; unmanned aircraft vehicles; Aerospace electronics; Aircraft propulsion; Automatic control; Automation; History; Military aircraft; Performance evaluation; Personnel; Testing; Unmanned aerial vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2005. Proceedings of the 2005
ISSN
0743-1619
Print_ISBN
0-7803-9098-9
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2005.1470516
Filename
1470516
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