New Pogo Analysis Method Using Rational Fitting and Three-Dimensional Tank Modeling-Reference-Cited by-同舟云学术

New Pogo Analysis Method Using Rational Fitting and Three-Dimensional Tank Modeling

Published:2015-02 Issue:2 Volume:53 Page:405-412
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Xu Deyuan¹,Hao Yu¹,Tang Guoan¹

Affiliation:

1. Department of Mechanics and Engineering Science, Fudan University, 200433 Shanghai, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053046

Reference22 articles.

1. CoppolinoR. N.LockM. H.RubinS., Space Shuttle Pogo Studies, NASA and Lyndon B.Johnson Space Center, Rept. NASA-CR-151596, Houston, TX, 1977, pp. 1–157.

2. A study of Saturn AS-502 coupling longitudinal structural vibration and lateral bending response during boost

3. Saturn V longitudinal oscillation (POGO) solution

4. Longitudinal instability of liquid rockets due to propulsion feedback /POGO/.

Cited by 14 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. EVALUATION OF THE SCATTER OF LIQUID LAUNCH VEHICLE POGO OSCILLATION AMPLITUDES DUE TO THE INFLUENCE OF THE SCATTER OF INTERNAL FACTORS;Kosmìčna nauka ì tehnologìâ;2024-06-09

2. Adaptive control design for active Pogo suppression based on vibration-acceleration feedback;Acta Astronautica;2024-01

3. Adaptive control design for active Pogo suppression of large strap-on liquid launch vehicles;Acta Astronautica;2023-05

4. Modeling of Pogo Vibration in Rockets with Staged Combustion Cycle Engine;Journal of Spacecraft and Rockets;2021-10-29

5. Enhanced Method for Analyzing Pogo Stability of Liquid Rockets with Uncertain-But-Bounded Parameters;Journal of Spacecraft and Rockets;2021-10-25