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Review of advanced guidance and control algorithms for space/aerospace vehicles
Cooperative Attack of Multiple Missiles Based on Optimal Guidance Law
SMC for Missile Systems Based on Back-Stepping and ESO Techniques
SMC for Missile Systems Based on Back-Stepping and ESO Techniques
Overview of Recent Research in Finite-Time and Cooperative Control of Flight Vehicles
Distributed Cooperative Control Design for Finite-Time Attitude Synchronization of Rigid Spacecraft
Finite-Time Formation Reconfiguration of Multiple Spacecraft with Collision Avoidance Problems
Coordination Control Design for Formation Reconfiguration of Multiple Spacecraft
Overview of Flight Vehicle Control
Attitude Control of Multiple Rigid Bodies with Uncertainties and Disturbances
Missile Guidance Laws Based on SMC and FTC Techniques
Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances
Missile Guidance Law Based on ESO Techniques
Finite-Time Attitude Stabilization for Rigid Spacecraft
Adaptive Attitude Tracking Control for Rigid Spacecraft with Finite-Time Convergence
Finite-Time Attitude Control for Rigid Spacecraft Based on Adaptive Super-Twisting Algorithm
Finite-Time Fault Tolerant Attitude Tracking Control for Rigid Spacecraft with Actuator Saturation
SMC for Attitude Tracking of Rigid Spacecraft with Disturbances
Adaptive Nonsingular Terminal SMC for Rigid Spacecraft
Finite-Time Attitude Control of Multiple Rigid Spacecraft Using Terminal Sliding Mode
Adaptive SMC for Attitude Stabilization in Presence of Actuator Saturation
The Descriptions of Flight Vehicle
Decentralized Finite-Time Attitude Synchronization and Tracking Control for Rigid Spacecraft
Coordination Control of Multiple Euler-Lagrange Systems for Escorting Mission
Distributed Fault-Tolerant Control Design for Spacecraft Finite-Time Attitude Synchronization
Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults