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INVERSE SIMULATION OF A HELICOPTER-TOWING CABLE-SONAR SYSTEM

机译:直升机牵引电缆声纳系统的逆模拟

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An inverse simulation algorithm based on an integration method is applied to a system formed by a submerged vehicle towed by a single main rotor helicopter by means of a massive, elastic cable. The problem is split into two phases: at each discretization time-step of the inverse simulation, the trajectory of the cable suspension point is derived first, which results into the submerged vehicle following the desired pattern in water; then the control variables for the helicopter are determined, which make the suspension point follow the trajectory obtained at the previous step, including cable tension as an additional load. The control action is then integrated forward in time for a fully coupled complete helicopter-cable-vehicle system model. Discrepancies in the results between the inverse solution and the forward simulation at the end of the time-step are compensated by (ⅰ) introducing a guidance term, which slightly modifies the desired variables at the following step, in order to maintain the towed vehicle on the desired trajectory, and (ⅱ) by an attitude control logic for the helicopter, which manages the variation of moments generated by cable tension. The method is demonstrated for a towed vehicle representative of a realistic sonar system.
机译:一种基于积分方法的逆模拟算法应用于通过由大量的弹性电缆通过单个主转子直升机牵引的浸没式车辆形成的系统。该问题分为两个阶段:在逆模拟的每个离散化时间步骤中,首先导出电缆悬架点的轨迹,这将在水中的所需图案之后进入浸没式车辆;然后为直升机的控制变量被确定,这使得悬挂点跟随在先前步骤中获得,包括电缆张力作为附加负载的轨迹。然后,控制动作在完全耦合的完整直升机 - 电缆系统模型的时间内集成了前进。在时间步骤结束时的逆解和正模之间的结果的差异由(Ⅰ)引入引导项,其在以下步骤中略微修改所需的变量,以保持牵引车辆由直升机的姿态控制逻辑的所需轨迹和(Ⅱ)管理电缆张力产生的矩的变化。该方法用于代表逼真的声纳系统的牵引车辆。

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