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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
Simplified adaptive estimation
Isaac Yaesh,Uri Shaked +1 more
TL;DR: A simplified adaptive scheme is suggested for the estimation of the state vector of linear systems driven by white process noise that is added to an unknown deterministic signal that is applied to the target acceleration estimation problem in a Theater Missile Defence scenario.
Journal ArticleDOI
Integrated guidance and control design based on a reference model
TL;DR: In this paper, an Integrated Guidance and Control (IGC) algorithm based on a reference model is proposed for a side-jet missile, incorporating the response characteristics of the missile control loop into the guidance loop.
Dissertation
Network enabled capability of remote operation:systems engineering and human factors
TL;DR: This thesis sets out to investigate the differences between using an automated system for re-tasking air-to-surface missiles in flight as opposed to assigning the task to a human operator, and the potential capabilities of the human operator that may use such a system.
Proceedings ArticleDOI
Multi-Missile Interception Integrating New Guidance Law and Game Theoretic Resource Management
TL;DR: In this paper, the authors fuse game theoretic resource management and a noise level related guidance law to existing missile defense system which is called differential game law type M (DGL/M).
Journal ArticleDOI
A Novel Integral Sliding Mode-Type Continuous Guidance Law With Autopilot Lag for Intercepting Non-Cooperative Maneuvering Targets
Yan Xiao-dong,Lyu Shi +1 more
TL;DR: The proposed integral sliding mode guidance law with the constraints of the line-of-sight angle and its rate for the interception of a non-cooperative maneuvering target can effectively attenuate an abrupt change in guidance commands during the terminal homing phase in the presence of uncertainties without prior information.