Suppression of Nonlinear Rotary Slosh Dynamics using the SLS Adaptive Augmenting Control System Demonstration on a Quadcopter Testbed
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Jing Pei | Andrew Puetz | Luke J. Miller | Camilo Duarte | Camilo A. Duarte | Jing Pei | Jing Pei | Camilo Duarte | Andrew Puetz
[1] Robert Hall,et al. Ares-I Bending Filter Design Using A Constrained Optimization Approach , 2008 .
[2] Jing Pei,et al. Demonstration of the Space Launch System Augmenting Adaptive Control Algorithm on a Quad-Rotor , 2018 .
[3] Helmut F. Bauer,et al. Stability Boundaries of Liquid-Propelled Space Vehicles with Sloshing , 1963 .
[4] Curtis E. Hanson,et al. In-Flight Suppression of a De-Stabilized F/A-18 Structural Mode Using the Space Launch System Adaptive Augmenting Control System , 2015 .
[5] Arthur L. Greensite,et al. Analysis and design of space vehicle flight control systems , 1970 .
[6] Tannen S. VanZwieten,et al. Robust, Practical Adaptive Control for Launch Vehicles , 2012 .
[7] J. Junkins,et al. Analytical Mechanics of Space Systems , 2003 .
[8] Jing Pei,et al. Demonstration of the Space Launch System Augmenting Adaptive Control Algorithm on Pole-Cart Platform , 2018 .
[9] Jing Pei,et al. Demonstration of Launch Vehicle Slosh Instability on Pole-Cart Platform , 2015 .
[10] Daniel D. Kana,et al. Validated spherical pendulum model for rotary liquid slosh , 1989 .
[11] Claire J. Tomlin,et al. Quadrotor Helicopter Flight Dynamics and Control: Theory and Experiment , 2007 .