DocumentCode :
2593375
Title :
Curved path approaches and dynamic interpolation
Author :
Jackson, Joseph W. ; Crouch, Peter E.
Author_Institution :
Honeywell Inc., Glendale, AZ, USA
fYear :
1990
fDate :
15-18 Oct 1990
Firstpage :
404
Lastpage :
408
Abstract :
The method of splines was applied to the control of linearizable dynamical systems such that an affine invariant cost functional (total energy) is minimized subject to discrete path constraints. CAGD (computer-aided geometric design) and optimal control methods were applied to derive reference trajectories for comparison with the dynamic results, and to determine intercept times for the waypoints. An acceptable trajectory was generated by the application of these methods to a difficult aircraft approach problem. It is suggested that a combination of finite element and spline techniques should eventually be suitable for solutions of practical dynamic interpolation problems considered in the literature
Keywords :
aerospace computing; aircraft control; control system CAD; finite element analysis; interpolation; optimal control; splines (mathematics); affine invariant cost functional; aircraft approach; computer-aided geometric design; curved path approach; discrete path constraints; dynamic interpolation; finite element analysis; intercept times; linearizable dynamical systems; optimal control; reference trajectories; splines; total energy; Aerospace engineering; Air traffic control; Aircraft; Airports; Control systems; Design engineering; Flexible manufacturing systems; Interpolation; Spline; Systems engineering and theory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location :
Virginia Beach, VA
Type :
conf
DOI :
10.1109/DASC.1990.111322
Filename :
111322
Link To Document :
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