Roll Coupling Effects on the Stability Margins for VEGA Launcher-Reference-Cited by-同舟云学术

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Roll Coupling Effects on the Stability Margins for VEGA Launcher

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Roux Christophe¹,Cruciani Irene¹

Affiliation:

1. ELV

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6630

Reference12 articles.

1. PhilipsW,H,"EffectofSteadyRollingonLongitudinalandDirectionalStability",NASATN1627,June1948.

2. 2Day,R.E."CouplingDynamicinAircraft:ahistoricalperspective",NASASpecialPublication,532,1997.

3. Roll torques produced by fixed nozzle solid rocket motors

4. 4Blakelock,J.H.,AutomaticControlofAircraftandMissiles,JohnWileyandSons,1991.

5. 5Greensite,A.L,AnalysisandDesignofSpaceVehicleFlightControlSystems,SpartanBooks,NewYork,1970.

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1. Launcher flight control design using robust wind disturbance observation;Acta Astronautica;2021-09

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3. Legacy recovery and robust augmentation structured design for the VEGA launcher;International Journal of Robust and Nonlinear Control;2019-04-16

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