The aim of this paper is attitude control of spacecraft utilizing nonlinear control feedback
linearization. Input-output linearization is a technique of feedback linearization theory. In this …

This paper presents a three-dimensional model for maneuvering of a spacecraft with
unactuated fuel slosh dynamics, and uses Lagrangian for multi-pendulum analogy to obtain …

Fuel sloshing is a critical problem in attitude control of spacerobots. This paper presents a
3D mathematical model to describe dynamic of fuel slosh in spacerobot's container. A multi …

In this paper, a nonlinear adaptive backstepping Lyapunov-based controller is designed for
spacecraft. Using the Lyapunov theory, the integrated adaptive backstepping controller …

In this paper, Immersion and Invariance based adaptive backstepping control technique is
proposed for an aerial robot. This aerial robot is a quadcopter which have nonlinear, multi …

In the space missions according to uncertainties in the satellite dynamics, and due to effects
of the uncertainties on satellites attitude control, an adaptive control is effective and useful …

Space robots control and the advantages of controllers for these robots are active research
topics. In this paper, a variety of control methods were used to control the space robots …

In this paper focused on design of a second order sliding mode controller for a fixed wing
airplane using real twisting algorithm. Simple sliding mode controller creates chattering in …

The problem of finding a planar two-impulse transfer orbit between two known elliptical
orbits that minimizes the total characteristic velocity of the transfer arc is examined. Using a …

Slosh dynamics could make some harmful changes in attitude parameters of space robots in
orbital maneuvering. So, its necessary to control this harmful phenomenon. This paper …