The present invention relates to an
active control method of
airplane course constrained point errors. The method comprises the following steps that: the step 1: a
position control actuating cylinder,a displacement sensor and a force measuring sensor are installed at a test
machine support portion course constrained point, wherein the
position control actuating cylinder and the displacement sensor form closed-
loop control, and the force measuring sensor monitors size of the stress of the test
machine support portion course constrained point in real time; the step 2, a course force control
active load point is selected at a non-checking portion of the test
machine, and the
position control actuating cylinder and the displacement sensor are installed to allow load of the
active load point to be transmitted to a course constrained point; and the step 3, the constrained point force measuring sensor and a selected non-checking portion course force control actuating cylinder form a closed-
loop control system to apply a course constrained
point target load to the force control actuating cylinder so as to convert passive load of the constrained point to
active load. Through construction of a closed-
loop control condition, the
active control method of
airplane course constrained point errors can actively control the course constrained point errors into corresponding load control precision, the control process can be automatically performed, and when the test is continuously operated, the control process can still have an
active control effect; and moreover, the load control precision is adjustable, the application is flexible and convenient, and the operation is simple.