This article proposes a continuous nonsingular terminal sliding-mode control with integral-
type sliding surface (CNTSMC-ISS) framework for disturbed systems, in which we consider …

Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the
integrated position and attitude control of spacecraft has attracted increasing attention and …

The feasibility of achieving complex underactuated control based on a single orbital thruster
with two inputs and six outputs is explored in this article. The study applies this control …

In this paper, a novel scheme is presented to estimate the uncertainty and disturbance of the
spacecraft system by a compensatory vector calculated online from the information of …

This article proposes a fixed-time fuzzy disturbance observer–based adaptive integral
sliding-mode spacecraft control scheme with consideration of input uncertainties and …

The high-accuracy attitude maneuvering problem for spacecraft systems is investigated. A
prescribed performance function and a shifting function are first employed to ensure the …

To solve the problem of communication delays and topology changes and achieve a high-
precision formation configuration control index in the flight control of SAR (synthetic aperture …

The spacecraft serves as an effective tool for the space exploration. The present study is
devoted to investigate the yaw attitude adjustment motion of the spacecraft influenced by the …

The development of attitude control systems in recent years have increasingly focused on
Fault Tolerant Control (FTC) capabilities to deal with sensor and actuator faults as well as …

In this paper, the TS fuzzy observer-based adaptive tracking control of the biological system
with stage structure is studied. First, a biological model with stage structure is established …