Stratospheric airship flight performance parameter estimation method and system
A technology of stratospheric airship and flight performance, applied in the field of aviation measurement and control
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[0061] Embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
[0062] Such as figure 1 As shown, the present invention provides a method for estimating the flight performance parameters of a stratospheric airship,
[0063] Make the airship enter a stable circling flight state;
[0064] Obtain the ground speed, attitude information and position information of the airship;
[0065] According to the ground speed, attitude information and position information of the airship, the flight performance parameters of the airship are estimated.
[0066] Such as figure 2 As shown, which is better, making the airship enter the stable circling flight state includes: fixing the main propeller speed and yaw control amount of the airship, so that the airship enters the circling flight state; when the fluctuation value of the flying height of the airship is less than the preset value, That is to say, it is considered to enter a ...
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