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Tactical and strategic missile guidance
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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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Survey of maneuvering target tracking: II. Ballistic target models
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Cramer-Rao bound for nonlinear filtering with Pd<1 and its application to target tracking
TL;DR: An approximation of the theoretical bound for practical applications, such as target tracking, where the number of sensor scans is large, is proposed and an application of the developed techniques to the well-known filtering problem of tracking a re-entry ballistic object is presented.
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Missile guidance laws based on pursuit-evasion game formulations
Vladimir Turetsky,Josef Shinar +1 more
TL;DR: In this paper two guidance laws are compared, both based on a pursuit-evasion differential game formulation, the first is a linear-quadratic one and the second one is formulated with bounded controls and the miss distance as the performance index.
Proceedings ArticleDOI
Vision-Based Obstacle Avoidance for UAVs
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