An integrated guidance and control (IGC) scheme based on global terminal sliding mode
control (GTSMC), backstep** control (BC), linear feedback (LF), dynamic surface control …

A novel impact angle constrained integrated guidance and control (IGC) scheme is
proposed with non-singular terminal sliding mode control (NTSMC) technique for missile to …

This article solves the fixed-time trajectory tracking problem for hypersonic flight vehicles
(HFVs) encountered with diverse actuator faults and asymmetric envelope constraints. In …

This paper investigates the problem of integrated guidance and control (IGC) law design
with impact angle and general field-of-view (FOV) constraints. Firstly, the IGC model for …

In this paper, a novel fast attitude adaptive fault-tolerant control (FTC) scheme based on
adaptive neural network and command filter is presented for the hypersonic reentry vehicles …

In this study, a discrete-time incremental backstep** (DTIBS) controller with an extended
Kalman filter (EKF) is proposed for unmanned aerial vehicles (UAVs) with unknown actuator …

Strap-down seeker is rigidly fixed onto the missile body, which results in detection
information being coupled to the missile's attitude and having a narrow field-of-view (FOV) …

A novel full state‐constrained integrated guidance and control (IGC) schema for aerial
interceptors under input saturation with tunnel‐prescribed performance is proposed. To …

This paper studies the tracking control problem of the air-breathing hypersonic vehicle
(AHV) subject to mismatched uncertainties. A novel model transformation is proposed for …

This work attempts to achieve precise tracking control for the longitudinal dynamics of
hypersonic flight vehicles (HFVs) without adopting universal approximators (eg, fuzzy logic …