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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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Proceedings ArticleDOI
A differential evolution tuned optimal guidance law
R. Thangavelu,S. Pradeep +1 more
TL;DR: In this paper, the authors propose a novel improvisation of the optimal guidance law using differential evolution (DE) that compensates the effects of these assumptions and increases the range of validity of OGL, treating the missile-target kinematics as a black box in which nothing is known except the input and the output.
Journal ArticleDOI
Impact Angle Constrained Suboptimal Terminal Guidance of Interceptors for Air Defence
TL;DR: In this paper, a suboptimal Model Predictive Spread Acceleration Guidance (MPSAG) law is proposed for terminal phase of air defense missiles with impact angle constraint, where the latax demand is purposefully spread over the available time to go ( t go ), which is done by parameterizing it with respect to t go as a straight line and parabola.
Proceedings ArticleDOI
A Miss Distance Study for Homing Missiles: Tail vs Canard Control
TL;DR: In this paper, the relative merits of tail versus canard control for homing missiles are discussed from a modeling perspective, and a simple but realistic model is created for each component and the simulation is then used to determine miss distance for deterministic engagements.
Proceedings ArticleDOI
Safer UAV Piloting: A Robust Sense-and-Avoid Solution for Remotely Piloted Quadrotor UAVs in Complex Environments
Min Wang,Holger Voos +1 more
TL;DR: This paper proposes a novel nonlinear vehicle control system which takes into account of sensor characteristics, an emergency evaluation policy and a novel optimization-based avoidance control strategy and the effectiveness of the proposed approach is demonstrated and validated in simulation with multiple moving objects.
Journal ArticleDOI
Biased optimal guidance law with specified velocity rendezvous angle constraint
TL;DR: In this article, a biased optimal guidance law based on a simplified mathematical model is deduced for interceptors engaging against invasion aircraft, which can achieve specified velocity rendezvous angle as well as zero terminal miss distance.