Given the few unsuccessful space missions in the past few decades, designing a fault-
tolerant spacecraft's attitude control has piqued the scientific and academic community's …

Research on uncertainty-oriented optimal attitude control of spacecraft with complex space
environments and multisource uncertainties is a research hotspot. Considering that the …

This article presents an energy-efficient constrained attitude control scheme with fixed-time
convergence for spacecraft. Although fixed-time control provides fast convergence of the …

The recently developed flexible lander offers a potential option for future asteroid landing
missions due to its advantages in suppression of rebound and overturning. The strong …

A predefined-time attitude stabilization for complex structure spacecraft with liquid sloshing
and flexible vibration is investigated under input saturation during orbital maneuver. First …

This article presents the design of a safe learning attitude controller, based on the Koopman
operator (KO), for rest-to-rest spacecraft attitude reorientation under angular velocity …

This paper investigates the attitude control system of a flexible satellite consisting of a rigid
main-satellite, a partially expanded coilable mast and a rigid sub-satellite. Multiple critical …

In this paper we address the optimized attitude command generation and robust inverse
optimal control design for the spacecraft attitude tracking with large angle slews. Firstly, with …

For the sake of achieving the high-accuracy and high-bandwidth attitude measurement and
control integration of flexible spacecraft, an integrated method based on a novel …

ATTITUDE reorientation is a process of controlling the attitude of a rigid spacecraft to the
desired orientation. It plays an important role in guaranteeing the success of on-orbit space …