[HTML][HTML] Robust optimal adaptive trajectory tracking control of quadrotor helicopter

M Navabi, H Mirzaei - Latin American Journal of solids and structures, 2017 - SciELO Brasil
This paper focuses on robust optimal adaptive control strategy to deal with tracking problem
of a quadrotor unmanned aerial vehicle (UAV) in presence of parametric uncertainties …

[HTML][HTML] Mathematical modeling and simulation of the earth's magnetic field: A comparative study of the models on the spacecraft attitude control application

M Navabi, M Barati - Applied Mathematical Modelling, 2017 - Elsevier
In this paper, the Earth's magnetic field models which are widely used in spacecraft attitude
control applications are modeled and extensively compared with a reference model. The …

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 …

Hierarchical Deep Reinforcement Learning for cubesat guidance and control

A Tammam, N Aouf - Control Engineering Practice, 2025 - Elsevier
Abstract Advancements in Reinforcement Learning (RL) algorithms and technologies have
opened up new possibilities for their use in autonomous spacecraft control. This work …

Fuzzy control of fuel sloshing in a spacecraft

M Navabi, A Davoodi - 2018 6th Iranian Joint Congress on …, 2018 - ieeexplore.ieee.org
This paper studies effect of fuzzy controller on fuel sloshing dynamics in orbital maneuvering
of the spacecraft. For this aim, a mathematical model of coupled dynamics of spacecraft and …

3D multi-pendulum model of slosh dynamics in a spacecraft

M Navabi, A Davoodi - 2017 8th International Conference on …, 2017 - ieeexplore.ieee.org
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 …

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 …

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 …

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 …