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

• المؤلفون الرئيسيون: Pushpangathan, Jinraj V., Bhat, M. Seetharama, Harikumar, Kandath
• مؤلفون آخرون: School of Electrical and Electronic Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2019
• الموضوعات: Engineering::Electrical and electronic engineering; Nano Air Vehicle; Gyroscopic Coupling
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/106668; http://hdl.handle.net/10220/50044; http://dx.doi.org/10.2514/1.C034280
• المؤسسة: Nanyang Technological University

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...