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