集成式液压平衡电磁发射装置的非线性建模及控制  

Nonlinear Modeling and Control of Integrated Hydraulic Balanced Electromagnetic Launch System

作　　者：聂世雄[1] Nie Shixiong(National Key Laboratory for Vessel Integrated Power System Technology Naval University of Engineering,Wuhan 430033 China)

机构地区：[1]海军工程大学舰船综合电力技术国防科技重点实验室,武汉430033

出　　处：《电工技术学报》2023年第4期852-864,共13页Transactions of China Electrotechnical Society

基　　金：国家自然科学基金面上资助项目(51977218)。

摘　　要：电磁发射系统的推力精确可调,使水下武器通用动力发射成为可能,但水下发射系统的动力学呈强非线性,增大了内弹道调节的难度。该文首先推导了液压平衡式水下发射系统的非线性动力学模型,然后运用反馈线性化将系统转化为伪线性系统,继而分别采用比例-积分-微分控制和滑模控制实现了内弹道的有效控制,同时与前馈控制进行了对比。结果表明,反馈线性化控制和前馈控制均取得了良好的效果,反馈线性化与比例-积分-微分的复合控制最适合水下电磁发射。The traditional underwater launch device uses high-pressure gas to launch the load, and the structure and timing of the gas-generating mechanism are solidified. It operates in an open-loop mode according to the preset parameters, and cannot be accurately adjusted in time according to the load state, so meeting the increasing and diversified launch requirements is challenging. The thrust of the electromagnetic launcher is precisely adjustable, which makes it possible to launch underwater weapons using universal power. The resistance of the ground electromagnetic launcher is mainly nonlinear sliding friction and aerodynamic resistance.In addition, the resistance is considered small compared with the thrust at medium and low speeds. Thus, the model of the ground electromagnetic launcher can be simplified to a linear control system. However, the fluid resistance of the hydraulically balanced electromagnetic launch system is large and has a strong nonlinear relationship with the flow rate. The additional mass increases continuously during the launch process, and the system cannot be simplified into a linear system, which makes internal ballistic adjustment more difficult.Based on the principle and structure of the hydraulically balanced electromagnetic launch device, this paper first deduces the nonlinear dynamic analytical equation of the system, and gives a detailed derivation of key variables, which makes the nonlinear characteristics of the system clearer. A lumped loss coefficient is adopted to represent all fluid losses in the launch system and is directly calculated using easily measurable parameters such as thrust, mover, and load velocities. The system is transformed into a pseudo-linear system using state feedback linearization. Considering the practical engineering factors, the composite control strategies of "feedback linearization + proportion integration differentiation(PID) control" and "feedback linearization + sliding mode control(SMC)" are adopted respectively based on classical PID control and SMC.

关 键 词：电磁发射 液压平衡 非线性模型 反馈线性化 

分 类 号：TM464[电气工程—电器]