The descent longitudinal trajectory control methodology of a hypersonic glider to carry out a
pullup maneuver is presented. A dynamic pole placement controller is implemented as the …

Considering the uncertainty of the flight dynamics model of the tilt‐rotor aircraft in different
flight modes, an L1 adaptive controller for full flight modes control system of tilt‐rotor aircraft …

In order to improve robust and tracking performance of aircraft controller, this paper presents
a design method of nonlinear controller for the longitudinal system of aircraft based on L1 …

This paper presents an analysis of the flight parameters and uncertainties that a HiFire 4–
like hypersonic glider experiences through a pull up and a bank maneuver along the …

This paper proposes a novel integrated guidance and autopilot (IGA) method for hypersonic
vehicles in dive phase. The third order back-step** L1 adaptive control is implemented to …

Aiming at the problems of high-frequency oscillation easily caused by the traditional model-
referenced adaptive control and the poor uncertainty and robustness of the traditional PID …

This paper presents an analysis of the modified L1 adaptive control law. The performance of
this control law is compared to the original control law. The modified L1 control law uses the …

This paper proposes a novel integrated guidance and control (IGC) method for hypersonic
vehicle in terminal phase. Firstly, the system model is developed with a second order …