Journal ArticleDOI
Analytical solution of optimal trajectory-shaping guidance
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This article is published in Journal of Guidance Control and Dynamics.The article was published on 1989-07-01. It has received 18 citations till now. The article focuses on the topics: Terminal guidance.read more
Citations
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Journal ArticleDOI
Design of Fuzzy Logic Guidance Law Against High-Speed Target
Chun-Liang Lin,Yung-Yue Chen +1 more
TL;DR: In this paper, an advanced guidance law is developed against very high-speed targets, where the aspect angle of the interceptor at lock-on near 180 degrees is a fundamental requirement for achieving small miss distance against a very high speed target.
Journal ArticleDOI
Analysis of optimal midcourse guidance law
TL;DR: In this paper, an optimal midcourse guidance law is presented that maximizes the final speed for missiles against a target at far distance or at low attitude in which the latter is a prime factor.
Journal ArticleDOI
Real-time neural-network midcourse guidance
Eunjung Song,Min-Jea Tahk +1 more
TL;DR: The advancement of the neural-network approach to the current level from the design procedure to the three-dimensional flight is described and is suitable for real-time implementation as well as generating suboptimal commands.
Journal ArticleDOI
Current Trends in Tactical Missile Guidance
S. Vathsal,A.K. Sarkar +1 more
TL;DR: A brief survey of the existing techniques and current trends in tactical missile guidance is presented in this paper, where the authors present a brief review of the current techniques and trends in this field.
References
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Journal ArticleDOI
Analysis of Optimal Evasive Maneuvers Based on a Linearized Two-Dimensional Kinematic Model
J. Shinar,D. Steinberg +1 more
Journal ArticleDOI
Analysis of Three-Dimensional Optimal Evasion with Linearized Kinematics
J. Shinar,Y. Rotsztein,E. Bezner +2 more
TL;DR: In this article, a linearized kinematic model is used to analyze the three-dimensional optimal missile avoidance with a 3D linearized model and the solution requires maximum load factor and the problem is reduced to optimal roll position control having two phases.
Journal ArticleDOI
Analytical solution of optimal trajectory-shaping guidance
C. F. Lin,L. L. Tsai +1 more
TL;DR: In this paper, a closed-loop, nonlinear optimal guidance law for three-dimensional flight for both the mid-course and terminal phases is presented, which can quickly modify the missile trajectory during midcourse guidance when the target direction changes.
Journal ArticleDOI
Optimal evasive tactics against a proportional navigation missile with time delay.
Gary L. Slater,William R. Wells +1 more
TL;DR: The optimal control for an evasive target in a particular pursuit-evasion conflict has been determined and the solution to an associated minimax type problem is indicated, viz., the choice of gain for the pursuer so as to minimize the (maximum) miss of the optimal evader.
Journal ArticleDOI
Proportional navigation vs an optimally evading, constant-speed target in two dimensions
Paul M. Julich,David A. Borg +1 more
Abstract: : The problem of evading a constant speed proportional navigation pursuer is considered. Both the evader and the pursuer are assumed to have limited lateral acceleration capabilities. A time lag is included in the pursuer's guidance system. The problem of evasion is formulated as an optimal control problem with the performance criterion being the range at the point of closest approach. The type of evasive maneuver is shown to be dependent upon the initial relative positions of the target and pursuer. Typical trajectories for the target and evader are illustrated. (Author)