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Set-point control method for air ship on constant-value wind interference stratosphere

A stratospheric airship, fixed-point control technology, applied in three-dimensional position/channel control and other directions, can solve the problems of airship fixed-point control wind interference, etc., achieve stable control performance, save energy, and achieve simple effects

Active Publication Date: 2015-05-27
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is: to provide a fixed-point control method for constant wind interference stratospheric airship, which solves the problem of airship fixed-point control wind interference

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  • Set-point control method for air ship on constant-value wind interference stratosphere
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  • Set-point control method for air ship on constant-value wind interference stratosphere

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Embodiment Construction

[0033] The following content further describes the technical solutions and implementation modes of the present invention in conjunction with the accompanying drawings.

[0034] 1) Assume that the wind speed and wind direction of the constant wind are: V w , x O =(x O ,y O ), X L =(x L ,y L ) are the target point of fixed-point hovering and the current position of the airship respectively. According to the wind direction and X O 、X L Calculate the current position of the airship to the specified route (a straight line that passes the target point and is consistent with the wind direction, such as figure 1 The straight line L shown in 1 ) side deviation dy.

[0035] dy = ( x O - x 1 ) ( y ...

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Abstract

The invention discloses a set-point control method for an air ship on a constant-value wind interference stratosphere. The method comprises the following steps: calculating deflections between the axial positions and the vertical positions of a current position of the airship and a target point position by a plane geometry method according to the current position of the airship, the target point position of set-point hovering, the wind direction and the wind speed; then calculating the deflection of the current axial position of the airship by a classical PID method according to the axial position, the wind speed, the lateral position and the direction of wind interference, and calculating the flying speed deflection, the lateral position deflection and an included angle between the head of the airship and the wind direction according to the current flying speed of the airship; adjusting the axial position and the lateral position of the airship and the flying speed of the airship until the airship flies to the preset target position. According to the set-point control method, the influence of constant-value wind interference is considered; by the adoption of the classical PID structural design, propulsion and yaw control channels of a position retaining controller are realized; the set-point control method is easy to implement and stable in control performance.

Description

technical field [0001] The invention belongs to the field of automatic control of airships. The invention specifically relates to a fixed-point control method for a constant-value wind disturbance stratospheric airship. Background technique [0002] An airship is a lighter-than-air aircraft that belongs to the aerostat category. It does not rely on aerodynamic force to provide lift like traditional aircraft, but mainly relies on buoyancy to provide static lift, so it can fly at low speeds, and even maintain long-term stability in the air. Fixed-point suspension means that it is relatively stationary relative to the ground, which enables it to be used as a platform for long-term observation and communication. Whether the stratospheric airship platform can be realized depends on the length of time the airship stays in the air, that is, whether it can always maintain the desired position; when the stratospheric airship is hovering at a fixed point, the most important thing is ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
Inventor 陈欣肖鸣超李春涛
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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