A Coupled Aeroelastic Model for Launch Vehicle Stability Analysis-Reference-Cited by-同舟云学术

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A Coupled Aeroelastic Model for Launch Vehicle Stability Analysis

Published:2010-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Orr Jeb¹

Affiliation:

1. SAIC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7642

Reference9 articles.

1. Lukens, D.,Schmitt,A.,and Broucek, G. "Approximate Transfer Functions for FlexibleBooster and Autopilot Analysis," WADD-TR-61-93,1961.

2. Rheinfurth, M.H. "Control-Feedback StabilityAnalysis," ABMA DA-TR-2-60,1960.

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

4. Garner, D."Control TheoryHandbook," NASATM-X-53036,1964.

5. Orr, J."FRACTALLinear Model Dynamics," NASAMSFC/EV41(TCD20090535A), April 29,2009.

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