范康健, 李更丰, 孙思源, 别朝红. 基于直升机优化调度的电力系统灾后快速恢复模型[J]. 电网技术, 2024, 48(10): 4021-4030. DOI: 10.13335/j.1000-3673.pst.2024.1279
引用本文: 范康健, 李更丰, 孙思源, 别朝红. 基于直升机优化调度的电力系统灾后快速恢复模型[J]. 电网技术, 2024, 48(10): 4021-4030. DOI: 10.13335/j.1000-3673.pst.2024.1279
FAN Kangjian, LI Gengfeng, SUN Siyuan, BIE Zhaohong. Fast Post-disaster Recovery Model of Power System Based on Helicopter Optimal Dispatching[J]. Power System Technology, 2024, 48(10): 4021-4030. DOI: 10.13335/j.1000-3673.pst.2024.1279
Citation: FAN Kangjian, LI Gengfeng, SUN Siyuan, BIE Zhaohong. Fast Post-disaster Recovery Model of Power System Based on Helicopter Optimal Dispatching[J]. Power System Technology, 2024, 48(10): 4021-4030. DOI: 10.13335/j.1000-3673.pst.2024.1279

基于直升机优化调度的电力系统灾后快速恢复模型

Fast Post-disaster Recovery Model of Power System Based on Helicopter Optimal Dispatching

  • 摘要: 小概率-高风险的极端事件发生频率呈上升趋势,电网安全问题愈发严峻,建立健全应对极端天气和自然灾害的电力应急响应机制迫在眉睫。为确保高电压等级骨干网架的安全运行,充分利用通用航空资源,提出了一种电力系统灾后快速恢复方法。首先针对直升机飞行特性以及航路三维特性,建立了直升机三维航路规划模型,包含最小离地高度约束、最大转弯距离约束和最大俯仰距离约束等。在此基础上建立了基于直升机优化调度的电力系统灾后快速恢复模型,模型以经济损失最小为目标,考虑停电损失和直升机调用成本;约束条件包含直升机维修路径约束、电力系统安全运行约束及故障线路状态耦合约束,考虑了直升机容量约束、航行里程约束使得模型更加贴切实际。算例测试采用改进的IEEE 30节点系统,展示了利用直升机进行灾后恢复的全过程,结果验证了所提模型的有效性。

     

    Abstract: high risk extreme events and increasingly severe power grid security problems, it is urgent to establish and improve the power emergency response mechanism to cope with extreme weather and natural disasters. To ensure the safe operation of high-voltage level backbone grids and make full use of general aviation resources, a fast post-disaster recovery methodology of the power system is proposed in the paper. Based on the characteristics of helicopters and flight paths, a three-dimensional flight path planning model for the helicopter is established, which contains the minimum ground clearance constraint, the maximum turning distance, and the pitch distance constraint. On this basis, a model for fast post-disaster recovery of power systems based on optimal helicopter dispatch is developed, aiming to minimize the economic loss, considering the outage loss and the helicopter dispatch cost. The constraints include helicopter maintenance path constraints, the power system safe operation constraints, and the fault line state coupling constraints. The model is more appropriate and practical considering helicopter load and flight mileage constraints. The improved IEEE 30-node system is used for case testing, and the results verify the validity of the proposed model and demonstrate the whole post-disaster recovery process using helicopters.

     

/

返回文章
返回