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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
Cooperative Multiple-Model Adaptive Guidance for an Aircraft Defending Missile
Vitaly Shaferman,Tal Shima +1 more
TL;DR: In this article, a cooperative guidance law for a defender missile protecting an aerial target from an incoming homing missile is presented, where the defender knows the future evasive maneuvers to be performed by the protected target and thus can anticipate the maneuvers it will induce on the incoming Homing missile.
Journal ArticleDOI
Nonlinear H∞ Robust Guidance Law for Homing Missiles
Ciann-Dong Yang,Hsin-Yuan Chen +1 more
TL;DR: In this paper, the authors proposed an H1 robust guidance law for Homing missiles with nonlinear kinematics in the homing phase, which can achieve performance robustness in the absence of target's s acceleration information and under variations of the initial conditions of engagement.
Journal ArticleDOI
Intercept-Angle Guidance
TL;DR: In this paper, a sliding-mode approach is used to implement the guidance concept in all aerial interception geometries: namely, head-on, tail-chase, and the novel head-pursuit.
Journal ArticleDOI
Impact-Angle-Constrained Suboptimal Model Predictive Static Programming Guidance of Air-to-Ground Missiles
Harshal B. Oza,Radhakant Padhi +1 more
TL;DR: In this paper, a nonlinear suboptimal guidance law is presented for successful interception of ground targets by air-launched missiles and guided munitions, which accurately satisfies terminal impact angle constraints in both azimuth as well as elevation simultaneously.
Journal ArticleDOI
Augmented Polynomial Guidance With Impact Time and Angle Constraints
TL;DR: To derive a state feedback command for the proposed law with terminal constraints on the impact time and angle, a polynomial function of the guidance command with three unknown coefficients is introduced, determined to satisfy the terminal impact angle constraint.