Effects of gyroscopic coupling and countertorque in a fixed-wing nano air vehicle

For the nonlinear equations of motion of the nano air vehicle, including the gyroscopic coupling and countertorque generated by the propulsion system, a linear state-space model is developed for analyzing the effects of gyroscopic coupling and countertorque on the dynamic behavior of the nano air ve...

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Bibliographic Details
Main Authors: Pushpangathan, Jinraj V., Bhat, M. Seetharama, Harikumar, Kandath
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2019
Subjects:
Online Access:https://hdl.handle.net/10356/106668
http://hdl.handle.net/10220/50044
http://dx.doi.org/10.2514/1.C034280
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Institution: Nanyang Technological University
Language: English