Control of Spin-Stabilized Spacecraft With Sloshing Fluid Stores | Citedby Results | J. Dyn. Sys., Meas., Control. | ASME Digital Collection

Skip to Main Content

Skip Nav Destination

Control of Spin-Stabilized Spacecraft With Sloshing Fluid Stores

J. Dyn. Sys., Meas., Control. Dec 1992, 114(4): 728-731 (4 pages)

This article has been cited by the following articles in journals that are participating in CrossRef Cited-by Linking.

Optimum fuzzy sliding mode control of fuel sloshing in a spacecraft using PSO algorithm

M. Navabi
A. Davoodi
M. Reyhanoglu

Acta Astronautica. January 2020, 167

Modeling and control of a nonlinear coupled spacecraft-fuel system

M. Navabi
A. Davoodi
M. Reyhanoglu

Acta Astronautica. January 2019, 162

Fuzzy Attitude Control of Spacecraft With Fuel Sloshing via Linear Matrix Inequalities

Lilit Mazmanyan
Mohammad A. Ayoubi

IEEE Transactions on Aerospace and Electronic Systems. January 2018, 54(5)

Design of Satellite Attitude Control System Considering the Interaction between Fuel Slosh and Flexible Dynamics during the System Parameters Estimation

Alain G. de Souza
Luiz C.G. de Souza

Applied Mechanics and Materials. January 2014, 706

Satellite Attitude Control System Design considering the Fuel Slosh Dynamics

Luiz Carlos Gadelha de Souza
Alain G. de Souza

Shock and Vibration. January 2014, 2014

Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics

Alain G. de Souza
Luiz C. G. de Souza

Mathematical Problems in Engineering. January 2014, 2014

Dynamics of Cilia-Based Microfluidic Devices

J. Kongthon
J.-H. Chung
J. J. Riley
S. Devasia

Journal of Dynamic Systems, Measurement, and Control. January 2011, 133(5)