An aircraft-mounted flight release separation process control method

Abstract

The invention provides an aircraft-mounted flight release separation process control method, which comprises the following steps: firstly, acquiring an aircraft overall parameter and a release separation parameter as design data, calculating a control rudder deviation angle and a start control time initial value required for keeping a separation attitude stable, and calculating and determining anattitude angle instruction value in a separation process; then designing an attitude angle control law according to a classic control method to form a launch separation control scheme after checking acontrol rudder deviation angle and a start control time initial value through separation dynamic trajectory simulation calculation, and finally checking the effectiveness of the scheme through MonteCarlo simulation. Compared with the prior art, the invention has the advantages that in the separation control design, the initial control surface deflection angle is increased for aerial carrier aerodynamic interference in the existing plane symmetric aircraft separation process, the problem of release separation safety of aircrafts with airfoils is effectively solved, meanwhile, the fastest separation attitude angle instruction is added in the separation process, the risk of collision with the aerial carrier is greatly reduced, and the throwing separation safety is improved.

Description

technical field [0001] The invention relates to a method for controlling the separation process of hanging and launching of a carrier aircraft, which is suitable for the field of control of external hanging and launching. Background technique [0002] The non-powered space-to-ground shuttle is the key field of high-tech aerospace development in the world at this stage. After the unremitting efforts of the aerospace powers, the symmetrical space-to-ground vehicle has made great progress in the verification of key technologies. However, the process of any technology forming a product and putting it into use is a tortuous scientific and technological exploration. Before the development of aerospace vehicles, the United States used aircraft such as the White Knight to carry out demonstration and verification tests of hanging flights to fully verify key technologies. For unpowered space-to-ground plane symmetric aircraft, hanging flight launch is a common key technology flight ve...

AI Technical Summary

Problems solved by technology

However, unlike axisymmetric missiles, plane-symmetric aircraft have more severe airborne aerodynamic interference problems. For plane-symmetric aircraft that rely on aerodynamic surface flight and control, the separation safety problem is more prominent. Effective flight control methods in the region are particularly important

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