高度对高空风筝发电系统动力学特性影响

邵垒; 杨家豪; 罗中; 李伯晟; 黄梓凇; 张盛

doi:doi:10.19912/j.0254-0096.tynxb.2024-2210

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高度对高空风筝发电系统动力学特性影响

更新时间：2026-07-22

- 高度对高空风筝发电系统动力学特性影响
- Vol. 47, Issue 4, Pages: 337-349(2026)
- 作者机构：
- 作者简介：
- 基金信息：
- DOI：doi:10.19912/j.0254-0096.tynxb.2024-2210
  CLC： TM614
- Online First：08 May 2026，
  
  Published：2026
- 稿件说明：
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邵垒, 杨家豪, 罗中, et al. 高度对高空风筝发电系统动力学特性影响[J]. 2026, 47(4): 337-349.
DOI：

邵垒, 杨家豪, 罗中, et al. 高度对高空风筝发电系统动力学特性影响[J]. 2026, 47(4): 337-349. DOI： doi:10.19912/j.0254-0096.tynxb.2024-2210.

摘要

为研究高度对高空风筝发电系统动力学特性影响

依据高度-密度-温度-风速函数建立高空风筝动力学修正模型

并结合Simulink建立基于高度修正的高空风筝动力学仿真模型

以实时求解高空风筝运行时的运动特性、飞行轨迹和发电功率等参数。研究结果表明：在高初始风速和大初始俯仰角条件下高度的修正对风筝发电系统的动力学特性有显著影响。在不同初始风速下

收缩阶段修正模型的峰值消耗功率与原模型相比增加7.63%~10.02%

而在同周期下总能量与原模型相比增加15.94%~21.61%

且初始风速越大

高度变化对风筝运动轨迹影响越显著;在不同初始俯仰角下

收缩阶段修正模型的峰值消耗功率与原模型相比增加4.84%~6.63%

而在同周期下总能量与原模型相比增加0.73%~7.79%

且初始俯仰角越大

高度变化对轨迹影响就越显著;在不同升阻比下

收缩阶段修正模型的峰值消耗功率与原模型相比增加2.85%~10.03%

在同周期下总能量与原模型相比增加了3.96%~15.81%。

Abstract

In order to study the influence of altitude on the dynamic characteristics of the high-altitude kite power generation system

the high-altitude kite dynamics correction model is established based on the altitude-density-temperature-wind speed function

and the high-altitude kite dynamics simulation model based on the correction of altitude is established by combining with Simulink

so as to solve in real time parameters such as the kinematic characteristics

the flight trajectory and the power generation during the operation of the high-altitude kite. The results show that the altitude has a significant effect on the dynamic characteristics of the kite power generation system under high initial wind speed and large initial pitch angle. Under different initial wind speeds

the peak power consumption of the contraction phase of modified model increases by 7.63% to 10.02% compared with the original model

and the total energy under the same cycle increases by 15.94% to 21.61% compared with the original model

and the larger initial wind speed

the more significant impact of altitude on trajectory. under different initial pitch angles

the peak power consumption of the contraction phase of modified model increases by 4.84% to 6.63% compared with the original model

and the total energy in the same cycle increases from about 0.73% to 7.79% compared with the original model

and the larger initial pitch angle

the more significant the impact of altitude on trajectory; under different lift-to-drag ratios

the peak power consumption of the contraction phase of modified model increases from about 2.85% to 10.03% compared with the original model

and the total energy in the same cycle increases by approximately 3.96% to 15.81% compared with the original model.

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