Single and diagonal double thrust failure assessment of quad-copter at starting

Author:

Kar Ray Debopoma,Roy Tamal,Chattopadhyay Surajit

Funder

Skyfi Education Labs Pvt. Ltd., Bangalore, India

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Condensed Matter Physics,Instrumentation

Reference31 articles.

1. A state space linearization mathematical model and simulation of a quadrotor umanned aerial vehicle in hover mode;Jenie;Int. J. Mech. Prod. Eng.,2018

2. M. Hedayatpour, M. Mehrandezh, F.J. Sharifi, A unified approach to configurstion-based dynamic analysis of quadcopters for optimal stability, in: F. (ED.): ‘Math.DS’, pp. 1–7.

3. Hybrid field oriented and direct torque control for sensor-less BLDC motors used in aerial drone;Carey;IET Power Elec.,2017

4. Measurement and modelling of the dynamic radar cross-section of an unmanned aerial vehicle;Guay;IET Radar, Sonar, Nav.,2018

5. LQR controller design for quad-rotor helicopters;Okyere;J. Eng.,2019

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