Demonstration of Launch Vehicle Slosh Instability on a Pole-Cart Platform-Reference-Cited by-同舟云学术

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Demonstration of Launch Vehicle Slosh Instability on a Pole-Cart Platform

Published:2015-06-18 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
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Author:

Pei Jing¹,Rothhaar Paul M.¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2712

Reference10 articles.

1. 1Bauer, H. “Fluid Oscillation in the Containers of a Space Vehicle and Their Influence Upon Stability,” Tech. Rep. TR R-187, NASA Technical Report, 1963.

2. 3Greensite, A. “Analysis and Design of Space Vehicle Flight Control Systems. VolumeVII. Attitude Control During Launch,” Tech. Rep. CR-826, NASA Contractor Report, July 1967.

3. STABILITY BOUNDARIES OF LIQUID-PROPELLED SPACE VEHICLES WITH SLOSHING

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3. Suppression of Nonlinear Rotary Slosh Dynamics using the SLS Adaptive Augmenting Control System Demonstration on a Quadcopter Testbed;AIAA Scitech 2019 Forum;2019-01-06

4. Simple Input Disturbance Observer-Based Control: Case Studies;Journal of Dynamic Systems, Measurement, and Control;2017-09-08

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