NDLI: Desired attitude angles design based on optimization for side window detection of Kinetic Interceptor

Content Provider	IEEE Xplore Digital Library
Author	Zhu Bo Quan Quan Cai Kaiyuan
Copyright Year	2008
Description	Author affiliation: Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing (Zhu Bo; Quan Quan; Cai Kaiyuan)
Abstract	In this paper the characters of pitch angle, yaw angle and roll angle of kinetic interceptor (KI) with side window during the terminal guidance process are discussed. In order to guarantee that KI is able to track target missile with high speed continually, a novel method to design the desired attitude angles is presented. Given an ellipse side window, the constraints from visibility, angle of attack and the angle of sideslip on attitude angles are analyzed and illustrated in inequalities. The existence of the solution to these inequalities is confirmed through analyzing a special solution. An object function is designed and a single-objective nonlinear optimization model is thereby formulated. The solutions of this optimization problem, which could be obtained through solving the optimization model, are regarded as the desired attitude angles. The initial value chosen to solve the problem by numerical iterative algorithm is also discussed. The validity of the analysis and the effectiveness of the method are confirmed by simulation results.
Starting Page	592
Ending Page	597
File Size	144616
Page Count	6
File Format	PDF
ISBN	9787900719706
DOI	10.1109/CHICC.2008.4605647
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2008-07-16
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute Of Intelligence M&C Technical Of KMUST
Subject Keyword	Missiles Accuracy Attitude control Kinetic interceptor Process control Nonlinear optimization Desired attitude angles World Wide Web Attitude tracking Distance measurement Optimization
Content Type	Text
Resource Type	Article

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