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Tactical and strategic missile guidance
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TLDR
In this paper, a three-loop Autopilot is used to provide tactical and strategic guidance for a single-antenna MIMO-BMG system using MATLAB units.Abstract:
Numerical Techniques Fundamentals of Tactical Missile Guidance Method of Adjoints and the Homing Loop Noise Analysis Convariance Analysis and the Homing Loop Proportional Navigation and Miss Distance Digital Fading Memory Noise Filters in the Homing Loop Advanced Guidance Laws Kalman Filters and the Homing Loop Other Forms of Tactical Guidance Tactical Zones Strategic Considerations Boosters Lambert Guidance Strategic Intercepts Miscellaneous Topics Ballistic Target Properties Extended Kalman Filtering and Ballistic Coefficient Estimation Ballistic Target Challenges Multiple Targets Weaving Targets Representing Missile Airframe with Transfer Functions Introduction to Flight Control Design Three-Loop Autopilot. Appendices: Tactical and Strategic Missile Guidance Software Converting Programmes to C Converting Programmes to MATLAB Units.read more
Citations
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Journal ArticleDOI
Three‐dimensional nonlinear H∞ guidance law
Ciann-Dong Yang,Hsin Yuan Chen +1 more
TL;DR: In this paper, the authors proposed a nonlinear H∞-guided missile guidance law for pursuit-evasion trajectories, which is expressed in a simple form by solving the associated Hamilton-Jacobi partial differential inequality analytically.
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Exo-Atmospheric Guidance of an Accelerating Interceptor Missile
Tal Shima,Oded M. Golan +1 more
TL;DR: It is shown that on top of enforcing a different flight geometry for the interceptor, the use of the new guidance to collision sliding mode guidance law can enhance the capture zone of the intercepted missile.
Journal ArticleDOI
Hyperbolic tangent function weighted optimal intercept angle guidance law
TL;DR: In this article, a new optimal guidance law with terminal constraints on miss distance and intercept angle is proposed for a missile with time-varying velocity against a maneuvering target.
Journal ArticleDOI
Fuzzy logic implementation of proportional navigation guidance
V. Rajasekhar,A.G. Sreenatha +1 more
TL;DR: In this paper, a Fuzzy Logic Controller (FLC) based on the popular Proportional Navigation Guidance (PNG) law is proposed in order to alter the value of the equivalent Navigational Constant to reap the maximum benefits in terms of the missile performance.
Journal ArticleDOI
Autonomous entry guidance using Linear Pseudospectral Model Predictive Control
TL;DR: Results demonstrate that the proposed autonomous entry guidance method has wide applicability, strong robustness, and excellent performance, and its computational efficiency is so high that it sufficiently satisfies the requirement on onboard application.