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    • 7. 发明申请
    • APPARATUS AND METHOD FOR CONTROLLING THE SHAPE OF STRUCTURES
    • 用于控制结构形状的装置和方法
    • WO1994026588A1
    • 1994-11-24
    • PCT/US1994005053
    • 1994-05-05
    • GRUMMAN AEROSPACE CORPORATIONAUSTIN, FredROSSI, Michael, J.KNOWLES, Gareth, J.
    • GRUMMAN AEROSPACE CORPORATION
    • B64C03/52
    • B64C3/48Y02T50/14
    • An apparatus and method control the shape of a structure (6) with one or more surfaces (8, 9) and internal actuators (11). A plurality of translational actuators (11) are capable of extending and contracting. The structure (6) can have any number of controllable surfaces (8, 9) which are controlled by computing the actuator strokes or loads required for achieving specified surface deflections. There are two methods for accomplishing this control. In the actuator stroke-control method, the surface deflections, or deflection errors for closed-loop control, are multiplied by a stroke-control gain matrix which is a function of the properties of the structure with the actuators absent. In the actuator load-control method, the surface deflections, or deflection errors for closed-loop control, are multiplied by a load-control gain matrix which is a function of the properties of the structure with the actuators absent. In either of these methods, different control gain matrices can be developed depending on whether it is desired to minimize actuator loads or surface shape errors.
    • 控制具有一个或多个表面(8,9)和内部致动器(11)的结构(6)的形状的装置和方法。 多个平移致动器(11)能够伸缩。 结构(6)可以具有任何数量的可控表面(8,9),其可通过计算用于实现指定的表面偏转所需的致动器行程或载荷来控制。 实现这种控制有两种方法。 在执行器行程控制方法中,闭环控制的表面偏转或偏转误差乘以行程控制增益矩阵,该行程控制增益矩阵是不存在执行器的结构特性的函数。 在执行器负载控制方法中,闭环控制的表面偏转或偏转误差乘以负载控制增益矩阵,该增益矩阵是不存在执行器的结构特性的函数。 在这些方法中的任一种中,可以根据是否希望最小化致动器负载或表面形状误差来开发不同的控制增益矩阵。