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灵活的太阳能阵列的非线性稳定性和振动在半阴影阶段在热诱导的动下
Omid Motaharifard1, Kamran Daneshjou1, Majid Bakhtiari2
1Department of Mechanical Engineering, Iran University of Science and Technology, Narmak, Tehran, 16844, Iran.
Scientific reports
|February 19, 2026
概括
这项研究模拟了带有灵活太阳能阵列的航天器,以了解热和自我激发的振荡. 它揭示了在轨道热变化期间,极限周期振荡和内部共振如何影响航天器动态.
科学领域:
- 太空飞船动力学和控制
- 结构动力学 结构动力学
- 航空航天工程 航空航天工程
背景情况:
- 具有灵活太阳能阵列的航天器由于热梯度而经历复杂的振动.
- 轨道机动期间的短暂的热条件,如半阴影阶段,可以诱导自我激发的振荡.
- 非线性现象,如极限周期振荡 (LCOs) 和内部共振对于航天器的稳定性至关重要.
研究的目的:
- 为具有灵活太阳能阵列的航天器开发非线性分析模型.
- 调查热模式下的振动现象,重点关注半阴影阶段.
- 分析灵活空间结构中的极限周期振荡 (LCOs) 和内部共振.
主要方法:
- 开发一种非线性分析模型,捕捉合的曲-曲-扭曲运动.
- 纳入短暂的热梯度和结构灵活性效应.
- 应用非线性动态建模,时间域模拟和模型缩小来导出非线性普通微分方程.
- 使用多个尺度 (MMS) 方法分析识别内部共振条件.
- 采用相位图,庞卡雷截面和分叉图来进行动态行为评估.
主要成果:
- 该模型成功捕捉了复杂的振动现象,包括LCO和内部共振.
- 通过分析识别了内部共振条件,澄清了模态能量交换.
- 分叉分析阐明了在不同的热条件下LCOs的出现和演变.
- 这项研究提供了对像哈勃太空望远镜这样的灵活空间结构特有的热力学不稳定性的见解.
结论:
- 开发的非线性模型为灵活的航天器的合热力学不稳定性提供了关键的见解.
- 了解LCO和内部共振对于设计强大的航天器系统至关重要.
- 这些发现有助于改进用于动态热环境的航天器设计,并提高任务可靠性.
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