Spacecraft quaternion based attitude input-output feedback linearization control using reaction wheels

M Navabi, MR Hosseini - 2017 8th International conference on …, 2017 - ieeexplore.ieee.org
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 …

Nonlinear optimal control of relative rotational and translational motion of spacecraft rendezvous

M Navabi, MR Akhloumadi - Journal of Aerospace Engineering, 2017 - ascelibrary.org
A nonlinear optimal control technique is utilized to address coupled relative rotational and
translational motion in spacecraft rendezvous. A new formulation of relative rotational …

[HTML][HTML] Analytic optimal control for multi-satellite assembly using linearized twistor-based model

M Atallah, M Okasha, O Abdelkhalik - Advances in Space Research, 2024 - Elsevier
This paper presents Guidance and Control (G&C) systems for multi-satellite assembly in
proximity operations. The systems utilize the twistor model, which is linearized through …

3D modeling and control of fuel sloshing in a spacecraft

M Navabi, A Davoodi - 2017 IEEE 4th International Conference …, 2017 - ieeexplore.ieee.org
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 …

Integrated adaptive backstepping attitude control of spacecraft

S Soleymanpour, M Navabi - 2017 IEEE 4th International …, 2017 - ieeexplore.ieee.org
In this paper, a nonlinear adaptive backstepping Lyapunov-based controller is designed for
spacecraft. Using the Lyapunov theory, the integrated adaptive backstepping controller …

Optimum design of robust adaptive controller with actuator constraints

M Navabi, H Mirzaei, A Davoodi - International Journal of Control …, 2020 - Springer
In this paper, a direct optimal adaptive nonlinear tracking control method for a class of
uncertain Multi-Input Multi-Output (MIMO) nonlinear systems with actuator amplitude …

Immersion and invariance based adaptive control of aerial robot in presence of inertia uncertainty

M Navabi, S Soleymanpour - 2017 IEEE 4th International …, 2017 - ieeexplore.ieee.org
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 …

A hybrid PSO fuzzy-MRAC controller based on EULERINT for satellite attitude control

M Navabi, S Hosseini - 2020 8th Iranian Joint Congress on …, 2020 - ieeexplore.ieee.org
This paper presents a new hybrid optimal fuzzy controller which is based on the reference
model modification of a model reference adaptive controller. The controller is applied to a …

Design of optimal adaptive control for satellite attitude in presence of uncertainty in moment of inertia

M Navabi, NS Hashkavaei - 2019 5th Conference on …, 2019 - ieeexplore.ieee.org
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 …

Adaptive feedback linearization control of space robots

M Navabi, S Hosseini - 2017 IEEE 4th International …, 2017 - ieeexplore.ieee.org
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 …