Vibration Suppression of an Underactuated Dynamic System Using Virtual Actuators

Author:

Khoshnood A. M.1,Azad I.2,Hasani S. M.2

Affiliation:

1. Assistant Professor Aerospace Engineering Department, K. N. Toosi University of Technology, P.O. Box 16765-3381, Tehran 16569-83911, Iran e-mail:

2. Aerospace Engineering Department, K. N. Toosi University of Technology, P.O. Box 16765-3381, Tehran 16569-83911, Iran e-mail:

Abstract

Sloshing is one of the critical problems in aerospace vehicles with liquid containers. Motion of the liquid in resonance situations can degrade the stability and performance of attitude control systems. Two important characteristics of this time varying phenomenon are sensorless and underactuated properties which lead to difficulty of attitude control system design. In this paper, a new technique based on soft sensor and virtual actuator is used to suppress the effects of fuel sloshing in an aerospace launch vehicle (ALV). For this purpose, a nonlinear dynamic model of the vehicle with mechanical model of the fuel sloshing is considered as a multibody dynamic system. The preliminary attitude control system of the vehicle is extended using the new vibration suppression technique and a numerical simulation of the nonlinear model is carried out. Results of the simulation show that the undesired effects of the fuel sloshing are effectively decreased using the proposed vibration suppression technique.

Publisher

ASME International

Subject

General Engineering

Reference23 articles.

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

5. Attitude Controller Design for a Launch Vehicle With Fuel-Slosh,2000

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