Optimum fuzzy sliding mode control of fuel sloshing in a spacecraft using PSO algorithm
M Navabi, A Davoodi, M Reyhanoglu - Acta astronautica, 2020 - Elsevier
This paper introduces an Optimal Fuzzy Sliding Mode (OFSM) controller for the control of
fuel sloshing in a spacecraft during orbital maneuvers. In order to optimize controller's gains …
fuel sloshing in a spacecraft during orbital maneuvers. In order to optimize controller's gains …
Advanced GNC-oriented modeling and simulation of Vertical Landing vehicles with fuel slosh dynamics
This paper introduces a flexible framework to enable high-fidelity simulations of the fuel
slosh dynamics for verification of the Guidance, Navigation and Control (GNC) algorithms …
slosh dynamics for verification of the Guidance, Navigation and Control (GNC) algorithms …
Modeling and control of a nonlinear coupled spacecraft-fuel system
M Navabi, A Davoodi, M Reyhanoglu - Acta Astronautica, 2019 - Elsevier
This paper considers the nonlinear interaction of the rigid body dynamics of a spacecraft
with the sloshing dynamics of the liquid propellant in its partially filled spherical tank during …
with the sloshing dynamics of the liquid propellant in its partially filled spherical tank during …
[HTML][HTML] Sparse Online Gaussian Process Adaptive Control of Unmanned Aerial Vehicle with Slung Payload
In the past decade, Unmanned Aerial Vehicles (UAVs) have garnered significant attention
across diverse applications, including surveillance, cargo shipping, and agricultural …
across diverse applications, including surveillance, cargo shipping, and agricultural …
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 …
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 …
of the uncertainties on satellites attitude control, an adaptive control is effective and useful …
FRIT-based integral action state feedback controller tuning using PSO for a liquid slosh suppression system
This paper presents a model-free approach of controller tuning to a liquid slosh suppression
system. The sloshing is the usual occurrence happening to the liquid in a moving container …
system. The sloshing is the usual occurrence happening to the liquid in a moving container …
Design of a robust controller using real twisting algorithm for a fixed wing airplane
M Navabi, N Davoodi - 2019 5th Conference on Knowledge …, 2019 - ieeexplore.ieee.org
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 …
airplane using real twisting algorithm. Simple sliding mode controller creates chattering in …
State Feedback Controller Tuning for Liquid Slosh Suppression System Utilizing LQR-LMI Approach
NN Zulkifli, MS Ramli - 2021 IEEE International Conference on …, 2021 - ieeexplore.ieee.org
This paper presents a tuning constraint optimization approach in state feedback controller
for liquid slosh suppression system. A suboptimal LQR method is employed to obtain the …
for liquid slosh suppression system. A suboptimal LQR method is employed to obtain the …
Nonlinear control of a space robot with slosh dynamics in two dimension
M Navabi, A Davoodi - 2018 6th RSI International Conference …, 2018 - ieeexplore.ieee.org
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 …
orbital maneuvering. So, its necessary to control this harmful phenomenon. This paper …