Energy Management Strategy for High-Altitude Solar Aircraft Based on Multiple Flight Phases

Table 3

The initial configuration parameters for model.

Parameters	Values	Units	Descriptions
	50	kg	Mass of aircraft
	6	kWh	Total power capacity of battery
	3.5	kWh	The initial electric quantity of battery
	22.5	m	Span length
	25.3	m^2	Wing area
	16.2	m^2	Area of solar cells