Distributed Modeling and Control of Large-Scale Highly Flexible Solar-Powered UAV

Table 1

The mass parameters of high aspect-ratio solar-powered UAV.

	Coefficient of mass	CG (from leading edge)	Elastic center
Structure	0.3	35%	35%
Solar array	0.15	45%	/
Propulsion system	0.5	0%	/
Payload	0.05	(at the CG of UAV)	/