This paper describes how Control Moment Gyroscopes (CMGs) can be used for stability augmentation to a thrust vectoring system for a generic Vertical Take-Off and Landing platform. The response characteristics of the platform which uses only thrust vectoring and a second configuration which includes a single-gimbal CMG array are simulated and compared for hovering flight while subject to severe air turbulence. Simulation results demonstrate the effectiveness of a CMG array in its ability to significantly reduce the agility requirement on the thrust vectoring system. Albeit simplifying physical assumptions on a generic CMG configuration, the numerical results also suggest that reasonably sized CMGs will likely be sufficient for a small hovering vehicle.
CMG-Augmented Control of a Hovering VTOL Platform
AIAA Guidance, Navigation, and Control Conference and Exhibit ; 2007 ; Hilton Head, SC, United States
2007-08-20
Aufsatz (Konferenz)
Keine Angabe
Englisch
Investigation of hovering control of VTOL transport
Engineering Index Backfile | 1964
|Thrust losses in hovering for jet VTOL AIRCRAFT
NTRS | 1966
|Hovering and low speed controllability of VTOL aircraft
Engineering Index Backfile | 1959
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