Deep reinforcement learning for six degree-of-freedom planetary landing
This work develops a deep reinforcement learning based approach for Six Degree-of-
Freedom (DOF) planetary powered descent and landing. Future Mars missions will require …
Freedom (DOF) planetary powered descent and landing. Future Mars missions will require …
Back-stepping active disturbance rejection control design for integrated missile guidance and control system via reduced-order ESO
S Xingling, W Honglun - ISA transactions, 2015 - Elsevier
This paper proposes a novel composite integrated guidance and control (IGC) law for
missile intercepting against unknown maneuvering target with multiple uncertainties and …
missile intercepting against unknown maneuvering target with multiple uncertainties and …
State-of-the-art integrated guidance and control systems in unmanned vehicles: A review
We comprehensively discuss state-of-the-art integrated guidance and control (IGC) systems,
in applications ranging from guided missiles to unmanned vehicles. Unlike separate …
in applications ranging from guided missiles to unmanned vehicles. Unlike separate …
[HTML][HTML] Adaptive block dynamic surface control for integrated missile guidance and autopilot
A novel integrated guidance and autopilot design method is proposed for homing missiles
based on the adaptive block dynamic surface control approach. The fully integrated …
based on the adaptive block dynamic surface control approach. The fully integrated …
Fixed-time ESO based fixed-time integral terminal sliding mode controller design for a missile
This paper studies a novel fixed-time extended state observer based fixed-time integral
terminal sliding mode controller for partial integrated guidance and control design. Firstly, a …
terminal sliding mode controller for partial integrated guidance and control design. Firstly, a …
Sensor-based robust incremental three-dimensional guidance law with terminal angle constraint
In this work, a robust incremental three-dimensional (3D) guidance law is proposed
considering terminal angle constraint against maneuvering targets. As a stepping stone, the …
considering terminal angle constraint against maneuvering targets. As a stepping stone, the …
Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control
Z Li, Q Dong, X Zhang, Y Gao - Aerospace science and technology, 2022 - Elsevier
An integrated guidance and control (IGC) scheme based on global terminal sliding mode
control (GTSMC), backstepping control (BC), linear feedback (LF), dynamic surface control …
control (GTSMC), backstepping control (BC), linear feedback (LF), dynamic surface control …
A new sliding mode control design for integrated missile guidance and control system
J Guo, Y Xiong, J Zhou - Aerospace Science and Technology, 2018 - Elsevier
A new sliding mode control algorithm for integrated guidance and control (IGC) system is
proposed in this paper. Firstly, the IGC model is established and the nonlinearities, target …
proposed in this paper. Firstly, the IGC model is established and the nonlinearities, target …
Impact angle constrained integrated guidance and control for maneuvering target interception
OWING to the stringent performance requirements, guidance and control design for tactical
missiles is still an area of active research. In modern missile guidance, the concept of …
missiles is still an area of active research. In modern missile guidance, the concept of …
Three dimensional impact angle constrained integrated guidance and control for missiles with input saturation and actuator failure
W Wang, S Xiong, S Wang, S Song, C Lai - Aerospace Science and …, 2016 - Elsevier
A three dimensional integrated guidance and control law with impact angle constraint is
developed, using the dynamic surface control and extended state observer techniques, for …
developed, using the dynamic surface control and extended state observer techniques, for …