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missiles
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keywords:(missiles)
Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle
Bounds on the Miss of Multiple-Model-Based Terminal Guidance Laws
Smooth Sliding Mode Control for Missile Interception with Finite-Time Convergence
Effect of Missile Turn Rate on Aircraft Susceptibility to Infrared-Guided Missile
Estimation Enhancement by Cooperatively Imposing Relative Intercept Angles
Distributed Guidance Law Design for Cooperative Simultaneous Attacks with Multiple Missiles
Cooperative Strategies for Optimal Aircraft Defense from an Attacking Missile
Cooperative Circular Guidance of Multiple Missiles: A Practical Prescribed-Time Consensus Approach
Impact of Acceleration on Miss Distance Parameter Estimation
Analytic Solutions of Generalized Impact-Angle-Control Guidance Law for First-Order Lag System
Effect of Environment Parameters on the Ablation of Hypersonic Missile Wing
Necessary Conditions for “Hit-to-Kill” in Missile Interception Engagements
Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint
Optimal Disturbance Attenuation Approach with Measurement Feedback to Missile Guidance
Fast Range and Time Estimator for Staged Ballistic Missiles
Bounds on the Miss of Radar-Guided Missiles with Discrete Guidance
Active Control of Aeroelastic Vibrations for Electromechanical Missile Fin Actuation Systems
Hybrid Switched Gain-Scheduling Control for Missile Autopilot Design
Guaranteed Smooth Trajectory Generation for Field-of-View Constrained Impact-Time Control
Rationalizable Strategies for the Navigator–Target–Missile Game
Dynamic-Escape-Zone to Avoid Energy-Bleeding Coasting Missile
Vector Guidance Approach to Three-Player Conflict in Exoatmospheric Interception
Connections Between Linear and Nonlinear Missile Autopilots via Three-Loop Topology
Nondominated Strategies for Cautious to Courageous Aerial Navigation
Thrust Integrated Trajectory Optimization for Multipulse Rocket Missiles Using Convex Programming
New Differential Geometric Guidance Strategies for Impact-Time Control Problem
Sliding-Mode-Based Missile-Integrated Attitude Control Schemes Considering Velocity Change
Performance Analysis of Composite Propellant Based on HTPB–DNCB
Continuous-Time Predictive Control-Based Integrated Guidance and Control
Optimal Cooperative Guidance Laws in a Multiagent Target–Missile–Defender Engagement
Exact Guidance Solution for Maneuvering Target on Relative Virtual Frame Formulation
Minimum-Effort Intercept Angle Guidance with Multiple-Obstacle Avoidance
Game-Based Safe Aircraft Navigation in the Presence of Energy-Bleeding Coasting Missile
Nonlinear Fault-Tolerant Control with Prescribed Performance for Air-Breathing Supersonic Missiles
Augmented Three-Loop Autopilot Structure Based on Mixed-Sensitivity Optimization
Cooperative Differential Games Guidance Laws for Imposing a Relative Intercept Angle
Target Evasion from a Missile Performing Multiple Switches in Guidance Law
Evaluation Model and Exact Optimization Algorithm in Missile–Target Assignment
Generalized Analysis of Biased Proportional Navigation Guidance with Fractional Power Error Feedback
Control of Separated Flow over Swept Missile Fin Using Pitching Oscillations
Greedy Target Assignment with Interference Constraints Between Defensive Weapons
Cooperative Guidance for Multiple Powered Missiles with Constrained Impact and Bounded Speed
Improvement of Delayed-Detached Eddy Simulation Applied to Separated Flow over Missile Fin
Solutions to the Aerodynamics-Driven Inverse Guidance Problem