Journal Of Guidance Control And Dynamics

Journal Of Guidance Control And Dynamics

制导控制与动力学杂志

  • 3区 中科院分区
  • Q1 JCR分区

高引用文章

文章名称 引用次数
Real-Time Optimal Control via Deep Neural Networks: Study on Landing Problems 20
Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costates 16
New Impact Time and Angle Guidance Strategy via Virtual Target Approach 13
Rotation-Matrix-Based Attitude Tracking for Multiple Flexible Spacecraft with Actuator Faults 13
Pseudospectral Convex Optimization for Powered Descent and Landing 13
Frequency Responses Identification from Multi-Axis Maneuver with Simultaneous Multisine Inputs 12
Propellant-Optimal Powered Descent Guidance 12
Observer-Based Fault-Tolerant Attitude Control for Spacecraft with Input Delay 11
Optimal Rocket Landing Guidance Using Convex Optimization and Model Predictive Control 10
Sliding-Mode Impact Time Guidance Law Design for Various Target Motions 10
Generic Smoothing for Optimal Bang-Off-Bang Spacecraft Maneuvers 10
Deviated Pure-Pursuit-Based Optimal Guidance Law for Imposing Intercept Time and Angle 9
Trajectory Design Employing Convex Optimization for Landing on Irregularly Shaped Asteroids 9
Exploration of Alternative State Vector Choices for Low-Thrust Trajectory Optimization 9
Dual-Quaternion-Based Spacecraft Autonomous Rendezvous and Docking Under Six-Degree-of-Freedom Motion Constraints 8
Adaptive Attitude Tracking with Active Uncertainty Rejection 8
Three-Dimensional Optimal Impact Time Guidance for Antiship Missiles 8
Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode 8
Robust Aircraft Trajectory Planning Under Wind Uncertainty Using Optimal Control 8
Command-Filtered Incremental Backstepping Controller for Small Unmanned Aerial Vehicles 8
Generalized hp Pseudospectral-Convex Programming for Powered Descent and Landing 7
Electric Sail Thrust Model from a Geometrical Perspective 7
Attitude Control of a Flexible Solar Sail in Low Earth Orbit 7
Unified Multiobjective Optimization Scheme for Aeroassisted Vehicle Trajectory Planning 7
Survey on Guidance Navigation and Control Requirements for Spacecraft Formation-Flying Missions 7
Stability and Control of Spinning Electric Solar Wind Sail in Heliostationary Orbit 7
Spacecraft Attitude Fractional Feedback Control Using Rotation Matrices and Exponential Coordinates 7
Incremental Sliding-Mode Fault-Tolerant Flight Control 7
Nonsingular Sliding-Mode Control for Field-of-View Constrained Impact Time Guidance 7
Circular Impact-Time Guidance 6
Heuristic and Optimized Sensor Tasking Observation Strategies with Exemplification for Geosynchronous Objects 6
Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools 6
Missile Guidance Law Based on New Analysis and Design of SDRE Scheme 6
Attitude Stabilization Using Two Parallel Single-Gimbal Control Moment Gyroscopes 6
Shipboard Landing Control Enabled by an Uncertainty and Disturbance Estimator 6
Effects of Structural Failure on the Safe Flight Envelope of Aircraft 6
Fuel-Optimal Rocket Landing with Aerodynamic Controls 6
Distributed Control Allocation for Spacecraft Attitude Takeover Control via Cellular Space Robot 6
Optimality of Error Dynamics in Missile Guidance Problems 5
Solution of a Pursuit-Evasion Game Using a Near-Optimal Strategy 5
Optimal Evading Strategies for Two-Pursuer/One-Evader Problems 5
Precise Attitude Control of Multirotary-Joint Solar-Power Satellite 5
Attitude Determination from Ellipsoid Observations: A Modified Orthogonal Procrustes Problem 5
Sensor Allocation for Tracking Geosynchronous Space Objects 5
Aircraft Damage Identification and Classification for Database-Driven Online Flight-Envelope Prediction 5
Kinematic Steering Law for Conically Constrained Torque-Limited Spacecraft Attitude Control 5
Biplane-Quadrotor Tail-Sitter UAV: Flight Dynamics and Control 5
Anti-Unwinding Attitude Control of Spacecraft with Forbidden Pointing Constraints 5
Sensing Wind from Quadrotor Motion 5
Impact Time Control with Generalized-Polynomial Range Formulation 5