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A Methodology towards Rotorcraft Piloting Autonomy for Approach on Moving Offshore Platforms

机译:旋翼飞行驾驶自主权的方法,以便在移动海上平台上实现方法

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Helicopter operation on moving offshore platforms poses a challenge in terms of human factors and flight control. Higher control modes are essential to relieve pilot workload and enable autonomous shipdeck recovery. This paper focuses on control laws for fully autonomous approach guidance from cruise to relative hover on a moving shipdeck. First, the engagement geometry of a typical helicopter-ship combination is described. An instrument-like procedure including arrival and approach phases is defined and the necessary conditions for successful guidance based on ground track, altitude and ground speed parameters are specified. Second, outer loop control laws for real-time generation of the flight path vector commands are developed. The control laws use state feedback from the helicopter-ship system. Control gains arc defined in terms of the distance to next waypoint to achieve smooth and gradual state tracking. Third, a model-based inner loop control is implemented to command the required collective, cyclic and pedal inputs for accurate flight path vector tracking, stabilization and axes cross-coupling compensation tasks. Simulation studies are performed using a comprehensive real-time capable helicopter flight mechanics code. Operational scenarios with nominal approach and steep approach profiles are simulated in still air and in wind up to 30 knots with gusts. Simulation results have demonstrated precise tracking of the shipdeck's position, course and speed with robustness to wind gusts and the feasibility to fly steep approaches.
机译:在移动海上平台上的直升机运行在人类因素和飞行控制方面对挑战构成了挑战。更高的控制模式对于缓解飞行员工作负载并实现自动运输恢复至关重要。本文侧重于控制法律,从巡航到相对悬停在移动船上的巡航中的指导。首先,描述了典型的直升机 - 船舶组合的接合几何形状。确定了包括到达和接近阶段的仪器类似程序,并指定了基于地面轨道,高度和地速参数的成功指导的必要条件。其次,开发了用于实时生成飞行路径矢量命令的外环控制规律。控制法使用直升机 - 船系统的状态反馈。控制收益在与下一个航点的距离方面定义以实现平滑且渐进状态跟踪的弧度。第三,实现了基于模型的内环控制,以命令用于准确飞行路径向量跟踪,稳定和交叉耦合补偿任务的所需集体,循环和踏板输入。使用综合实时的直升机飞行机械代码进行仿真研究。具有标称方法和陡峭方法轮廓的操作场景在仍然空气中模拟,阵风最多30节。仿真结果表明,对船舶的位置,课程和速度具有精确的追踪,以鲁棒阵风和飞行陡峭方法的可行性。

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