Fixed-time ESO based fixed-time integral terminal sliding mode controller design for a missile

L Cui, N **, S Chang, Z Zuo, Z Zhao - ISA transactions, 2022 - Elsevier
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 …

Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstep** 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), backstep** control (BC), linear feedback (LF), dynamic surface control …

Impact angle constrained integrated guidance and control for maneuvering target interception

S He, T Song, D Lin - Journal of Guidance, Control, and Dynamics, 2017 - arc.aiaa.org
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 …

3-D impact angle constrained distributed cooperative guidance for maneuvering targets without angular-rate measurements

XH Wang, CP Tan - Control Engineering Practice, 2018 - Elsevier
In this paper, a three-dimensional (3-D) distributed cooperative guidance scheme is
presented for multiple missiles to attack a single maneuvering target at pre-specified impact …

Capturability of a sliding-mode guidance law with finite-time convergence

KB Li, HS Shin, A Tsourdos - IEEE Transactions on Aerospace …, 2019 - ieeexplore.ieee.org
Using the Lyapunov-like approach, the capturability of a recently proposed sliding-mode
guidance law, which is used for exoatmospheric interception and can guide the line-of-sight …

Nonlinear guidance laws for maneuvering target interception with virtual look angle constraint

Y Wang, H Wang, D Lin, W Wang - IEEE Transactions on …, 2021 - ieeexplore.ieee.org
For the problem of intercepting a maneuvering target with a desired terminal impact angle,
we propose a guidance law in this article based on a nonlinear relative virtual guidance …

[HTML][HTML] Integrated guidance and control of guided projectile with multiple constraints based on fuzzy adaptive and dynamic surface

S Jiang, F Tian, S Sun, W Liang - Defence Technology, 2020 - Elsevier
Based on fuzzy adaptive and dynamic surface (FADS), an integrated guidance and control
(IGC) approach was proposed for large caliber naval gun guided projectile, which was …