DocumentCode :
3334629
Title :
Motion planning for reduced observability of autonomous aerial vehicles
Author :
McFarland, Michael B. ; Zachery, Randy A. ; Taylor, Brian K.
Author_Institution :
Munitions Directorate, Air Force Armament Lab., Eglin AFB, FL, USA
Volume :
1
fYear :
1999
fDate :
1999
Firstpage :
231
Abstract :
Techniques originally developed for robot motion planning are applied to compute ingress paths for autonomous air vehicles, such as cruise missiles or uninhabited aerial vehicles (UAVs). This approach is particularly useful in multiobjective optimization problems such as intercepting a target while also maneuvering to minimize observability to ground-based tracking stations. Prescribing position and dimensional are chosen based on empirical measurements of the airframe´s radar cross-section (RCS) as well as target state information. This six-degree-of-freedom motion planning formulation is an alternative to the traditional separation of guidance and autopilot functions and results in an unprecedented degree of guidance and control subsystem integration. This paper presents preliminary results and lays the groundwork for the development of future highly integrated guidance and control systems
Keywords :
aircraft control; missile control; observability; path planning; radar cross-sections; autonomous aerial vehicles; autopilot functions; cruise missiles; ground-based tracking stations; ingress paths; motion planning; multiobjective optimization problems; radar cross-section; reduced observability; subsystem integration; target state information; uninhabited aerial vehicles; Missiles; Mobile robots; Motion planning; Observability; Path planning; Radar tracking; Remotely operated vehicles; Robot motion; Target tracking; Unmanned aerial vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Conference_Location :
Kohala Coast, HI
Print_ISBN :
0-7803-5446-X
Type :
conf
DOI :
10.1109/CCA.1999.806181
Filename :
806181
Link To Document :
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