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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
Aerial vehicle guidance based on passive machine learning technique
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A Target/Missile Engagement Scenario Using Classical Proportional Navigation
TL;DR: In this article, the authors deal with a simulation of a missile versus target engagement scenario, where a forward time solution of the two dimensional problem is developed which is converted to an adjoint model.
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Guidance Law Design Using Intelligent Non-Linear Controller
TL;DR: Simulation results show the effectiveness of the proposed missile guidance law against different engagement scenarios and the proposed controller gives good system performance in the face of system parameters variation and external disturbances.
Journal ArticleDOI
Multi-model approaches to three-axis missile autopilot design under aerodynamic roll angle uncertainty
TL;DR: In this article, the problem of designing a robust three-axis missile autopilot that operates under aerodynamic roll angle uncertainty is addressed, and two design methods with multi-objective output-feedback control are proposed.
Book ChapterDOI
Optimal fuzzy CLOS guidance law design using ant colony optimization
TL;DR: The well-known ant colony optimization meta-heuristic is applied to design a new command to line-of-sight guidance law and the parameters of a pre-constructed fuzzy sliding mode controller are optimized.