Abstract: The paper develops a noncertainty-equivalence adaptive (NCEA) spacecraft formation control system, using filtered signals, based on the immersion and invariance methodology. It is assumed that a target spacecraft is in an ...

Abstract: In this paper, an

Abstract: This paper presents the design of a higher-order sliding-mode control system for the three-axis attitude control of spacecraft using solar-radiation pressure in a finite time. The spacecraft, equipped with four solar plates, ...

Abstract: This paper presents the design of a higher-order sliding-mode control system for the three-axis attitude control of spacecraft using solar-radiation pressure in a finite time. The spacecraft, equipped with four solar plates, ...

Abstract: This paper develops a composite adaptive control law for the stabilization and parameter identification of a two-degree-of-freedom aeroelastic system, which is equipped with leading- and trailing-edge flaps. The multiple-input ...

Abstract: This paper addresses the development of control systems for the orbit control of spacecraft around irregularly shaped rotating asteroids with uncertain parameters. The objective is to steer the spacecraft along prescribed ...