Author:
Xi Leiping,Zhang Dizhou,Yang Sen
Reference6 articles.
1. Xi, L., Zhu, Q., Zhang, D.: Sliding mode control design based on fuzzy reaching law for yaw angle of a Tail-sitter UAV. In: 2016 22nd International Conference on Automation and Computing, Colchester, United Kingdom, vol. 09, pp. 238–243 (2016)
2. Stone, H.: Aerodynamic modelling of a wing-in-slip—stream tail-sitter UAV. In: 2002 Biennial International Powered Lift Conference and Exhibit, Williamsburg, 5–7 Nov 2002
3. Hugh Stone, R.: The T-wing tail-sitter research UAV. In: 2002 Biennial International Powered Lift Conference and Exhibit, pp. 1–10 (2002)
4. Mengzhao, L.: Moment of inertia of aircraft and its estimation. J. Aircr. Des. 3, 13–20 (1997)
5. Etkin, B., Reid, L.D.: Dynamics of Flight Stability and Control. Wiley (1996)