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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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Proceedings ArticleDOI
Trajectory Modulation Guidance Law for Anti-ship Missiles
TL;DR: A new optimal homing guidance law with terminal angle constraints is developed to improve the survivability of anti-ship missiles and a new virtual state variable is introduced to provide one more degree of freedom resulting in weave manoeuvres on the missile trajectory.
Proceedings ArticleDOI
Seeker Based Optimal Guidance Law, A Few Issues
TL;DR: Zarchan’s formula of just stable IGL is modified for minimum control margin of IGL, and if time constants for OGL is selected with stability margin formula based on higher navigation gain, somewhat longer seeker range will assure guidance performance without making radome slope specification too stringent to be peacticable.
Journal ArticleDOI
Continuous Robust Guidance Law for Intercepting Maneuvering Targets
Shaoming He,Defu Lin +1 more
Journal ArticleDOI
Adaptive Backstepping Impact Angle Guidance Law Accounting for Autopilot Lag
Shaoming He,Wei Wang,Defu Lin +2 more
TL;DR: In this paper, a robust impact angle guidance law for maneuvering target interception with autopilot dynamics compensation based on a systematic backstepping control technique is presented, which is based on the systematic back stepping control technique.
Journal ArticleDOI
Impact-time-control guidance laws for cooperative attack of multiple missiles
TL;DR: A new closed-form ITCG guidance solution is presented, based on the linear formulation, employ- ing base trajectories driven by PNG with various navigation constants that demonstrates the performance and feasibility of the proposed ITCGs law.