Analytical Investigation of Propellant Slosh Stability Boundary on a Space Vehicle-Reference-Cited by-同舟云学术

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Analytical Investigation of Propellant Slosh Stability Boundary on a Space Vehicle

Published:2021-09 Issue:5 Volume:58 Page:1514-1521
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Pei Jing¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A35024

Reference7 articles.

1. Saturn AS-501/S-IC flight control system design.

2. GreensiteA. L. “Analysis and Design of Space Vehicle Flight Control Systems, Volume VII—Attitude Control During Launch,” NASA CR-826, 1967, pp. 41–46.

3. BeerF. P.JohnstonR., Static and Dynamics, 6th ed., McGraw–Hill, Boston, MA, 1997, pp. 915–917.

4. WieB., Space Vehicle Dynamics and Control, 2nd ed., AIAA Education Series, AIAA, Reston, VA, 1998, pp. 503–512.

Cited by 3 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. Responsive tolerant control: An approach to extend adaptability of launch vehicles;Progress in Aerospace Sciences;2024-08

2. Effects of Propellant Slosh on Touchdown Stability for Landing Vehicles;Journal of Spacecraft and Rockets;2023-11-29

3. Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity;2022 IEEE 61st Conference on Decision and Control (CDC);2022-12-06

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