NDLI: Generalized model predictive static programming and its application to 3D impact angle constrained guidance of air-to-surface missiles

Content Provider	IEEE Xplore Digital Library
Author	Maity, A. Oza, H.B. Padhi, R.
Copyright Year	2013
Description	Author affiliation: Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India (Maity, A.; Oza, H.B.; Padhi, R.)
Abstract	A new `generalized model predictive static programming (G-MPSP)' technique is presented in this paper in the continuous time framework for rapidly solving a class of finite-horizon nonlinear optimal control problems with hard terminal constraints. A key feature of the technique is backward propagation of a small-dimensional weight matrix dynamics, using which the control history gets updated. This feature, as well as the fact that it leads to a static optimization problem, are the reasons for its high computational efficiency. It has been shown that under Euler integration, it is equivalent to the existing model predictive static programming technique, which operates on a discrete-time approximation of the problem. Performance of the proposed technique is demonstrated by solving a challenging three-dimensional impact angle constrained missile guidance problem. The problem demands that the missile must meet constraints on both azimuth and elevation angles in addition to achieving near zero miss distance, while minimizing the lateral acceleration demand throughout its flight path. Both stationary and maneuvering ground targets are considered in the simulation studies. Effectiveness of the proposed guidance has been verified by considering first order autopilot lag as well as various target maneuvers.
Starting Page	4999
Ending Page	5004
File Size	284638
Page Count	6
File Format	PDF
ISBN	9781479901777
ISSN	07431619
e-ISBN	9781479901784
DOI	10.1109/ACC.2013.6580614
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2013-06-17
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	American Automatic Control Council(AACC)
Subject Keyword	History Missiles Acceleration Optimal control Atmospheric modeling Azimuth Vehicle dynamics Computationally Efficient Optimal Control Generalized Model Predictive Static Programming Impact Angle Constrained Guidance
Content Type	Text
Resource Type	Article
Subject	Electrical and Electronic Engineering

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