1. Thakar, P. S., Bandyopadhyay, B., Gandhi, P. S., and Kurode, S., 2012, “Robust Control of Rotary Slosh Using Integral Sliding Modes,” 12th IEEE Workshop on Variable Structure Systems, VSS'12, Mumbai, India, Jan. 12–14, pp. 440–445.10.1109/VSS.2012.6163542
2. Hervas, J. R., and Reyhanoglu, M., 2012, “Control of a Spacecraft With Time-Varying Propellant Slosh Parameters,” 12th International Conference on Control, Automation and Systems, Jeju Island, Korea, Oct. 17–21, pp. 1621–1626.http://ieeexplore.ieee.org/xpl/login.jsp?tp=&arnumber=6393100&url=http%3A%2F%2Fieeexplore.ieee.org%2Fxpls%2Fabs_all.jsp%3Farnumber%3D6393100
3. Le-Mei, Z., Bao-Zeng, Y., Fang, X., Qun-Feng, X., and Xiao-Qiang, S., 2013, “Dynamic Inversion Control of Liquid-Filled Spacecraft Attitude and Fuel Sloshing Suppression,” 32th Chinese Control Conference, Xian, China, July 26–28, pp. 363–368.http://ieeexplore.ieee.org/xpl/login.jsp?tp=&arnumber=6639458&url=http%3A%2F%2Fieeexplore.ieee.org%2Fxpls%2Fabs_all.jsp%3Farnumber%3D6639458
4. Cho, S., and McClamrocht, N. H., 2000, “Feedback Control of a Space Vehicle With Un-Actuated Fuel Slosh Dynamics,” AIAA Paper No. 2000-4046.10.2514/6.2000-4046
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