Modeling and Adaptive Attitude Control of Aircraft with Varying Mass in Aerial Refueling-Reference-Cited by-同舟云学术

Modeling and Adaptive Attitude Control of Aircraft with Varying Mass in Aerial Refueling

Published:2021-10-30 Issue: Volume: Page:1907-1918
ISSN:1876-1100
Container-title:Lecture Notes in Electrical Engineering
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Author:

Zheng Wenxuan,Wang Honglun

Publisher

Springer Singapore

Link

https://link.springer.com/content/pdf/10.1007/978-981-15-8155-7_160

Reference15 articles.

1. Mao, W., Eke, F.: A survey of the dynamics and control of aircraft during aerial refueling. Nonlinear Dyn. Syst. Theory 8(4), 375–388 (2008)

2. Roskam, J.: Airplane flight dynamics and automatic flight controls. 1998: DARcorporation

3. Mao, W., Eke, F.: Effects of Mass variation on the motion of receiver aircraft during in-flight refueling. Int. Rev. Aerosp. Eng. (IREASE) 5(3), 109–116 (2012)

4. Guo, J., et al.: Modeling and control of UCAV with varying mass in autonomous aerial refueling. Flight Dyn. 29(6), 36–40 (2011)

5. Venkataramanan, S., Dogan, A.: Dynamic Effects of trailing vortex with turbulence & time-varying inertia properties in aerial refueling. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit (2004)

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