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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
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Journal ArticleDOI
A Terminal Guidance Law Based on Motion Camouflage Strategy of Air-to-Ground Missiles
TL;DR: In this paper, a guidance law for attacking ground targets based on motion camouflage strategy is proposed, and a two-dimensional and three-dimensional guidance law is derived by bringing the estimation for target maneuver.
Journal ArticleDOI
Distributed receding horizon filtering for mixed continuous-discrete multisensor linear stochastic systems
Il Young Song,Vladimir Shin +1 more
TL;DR: The derivation of the error cross-covariance equations between the LRHKFs in order to compute the optimal matrix weights makes the proposed distributed filter robust against dynamic model uncertainties.
Integrated Autopilot and Guidance for Dual Control Missiles Using Higher Order Sliding Mode Control
TL;DR: An integrated Autopilot-and Guidance Algorithm developed using Higher Order Sliding Mode Control, for interceptors steered by combination of aerodynamic lift, sustainer thrust and center of gravity divert thrusters, which also includes seeker tracker, bore sight stabilization and estimation of target lateral acceleration.
Proceedings ArticleDOI
Distribution of terminal cost functional in continuous-time controlled system with noise-corrupted state information
TL;DR: In this paper, the cumulative distribution function of the terminal cost in a scalar linear continuous-time system with noise corrupted measurements is derived, subject to a linear saturated control strategy.
Proceedings ArticleDOI
Research on Trajectory Scheme with Large Impact Angle for Fire-and-Forget Anti-Tank Missiles
TL;DR: In this article, a top attack trajectory of the anti-tank missile was designed, the missile flies out of the tube without control, the climb stage was completed by the index number regulation, the stage of glide at a certain angle of attack, at the end of the trajectory the guidance law which was deduced was adopted to satisfy the impact position and angular constraint.