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State Space System Modelling of a Quad Copter UAV

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arxiv 1908.07401 v2 pith:H7AOI73B submitted 2019-08-20 cs.RO

classification cs.RO
keywords copterquaddegreesfreedommodelsspacestatesystem
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In this paper, a linear mathematical model for a quad copter unmanned aerial vehicle (UAV) is derived. The three degrees of freedom (3DOF) and six degrees of freedom (6DOF) quad copter state-space models are developed starting from basic Newtonian equations. These state space models are very important to control the quad copter system which is inherently dynamically unstable.

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Cited by 1 Pith paper

Reviewed papers in the Pith corpus that reference this work. Sorted by Pith novelty score. Full citation record

  1. Integrated Sensing, Communication, and Over-The-Air Control of UAV Swarm Dynamics

    eess.SP 2025-02 conditional novelty 6.0 of 10

    A single base station can jointly perform over-the-air coordinated UAV control and object sensing on the same spectrum by designing BS-side post-processing and precoding matrices.

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