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Aircraft gliding deceleration control method

A technology for deceleration control and aircraft, applied in the direction of non-electric variable control, height or depth control, control/adjustment system, etc., to achieve the effects of high speed control accuracy, increased resistance, and effective speed control

Inactive Publication Date: 2016-08-10
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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AI Technical Summary

Problems solved by technology

[0003] However, the prior art has not been able to provide an effective and high-precision aircraft glide deceleration control method, so this problem needs to be solved urgently

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  • Aircraft gliding deceleration control method
  • Aircraft gliding deceleration control method
  • Aircraft gliding deceleration control method

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Embodiment Construction

[0032] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and examples.

[0033] This embodiment provides a control method for gliding deceleration of an aircraft, which is applicable to lift-type aircraft mainly based on aerodynamic flight, so as to solve the problem of high-precision speed control of the aircraft in a balanced gliding flight state.

[0034] figure 1 It is a schematic flow chart of the aircraft glide deceleration control method in the embodiment of the present invention. like figure 1 As shown, the aircraft glide deceleration control method in the embodiment of the present invention includes: .

[0035] Step 101, according to the instruction speed V given by the guidance system cx The current velocity V of the aircraft relative to the earth obtained by the navigation system d to determine whether deceler...

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Abstract

The invention discloses an aircraft gliding deceleration control method. The method comprises steps that whether deceleration control is needed is determined according to a difference value of an instruction speed Vcx provided by a guidance system and a motion speed Vd of an aircraft relative to the Earth acquired by a navigation system; if yes, a required basic attack angle alpha0 is acquired through calculation; a dissipation speed deltaV is acquired through calculation; a required deceleration attack angle alphan is acquired through calculation; an additional guidance force Fzc<V> for deceleration control is acquired through calculation; deceleration control on the aircraft is carried out according to the additional guidance force for deceleration control acquired through calculation. Through the method, precise speed control on the aircraft can be realized.

Description

technical field [0001] The invention relates to the technical field of hypersonic vehicle guidance, in particular to a control method for gliding deceleration of the vehicle. Background technique [0002] For the lift aircraft, because it mainly relies on aerodynamic flight, under the influence of uncertain factors and interference conditions, the velocity dispersion of the aircraft at the end of the flight is large, which is unfavorable to the subsequent flight. In order to constrain the velocity distribution of the terminal point, it is necessary to Strict speed control is carried out so that the speed tends to be consistent under disturbance conditions. [0003] However, an effective and high-precision aircraft glide deceleration control method has not yet been provided in the prior art, so this problem needs to be solved urgently. Contents of the invention [0004] In view of this, the present invention provides a method for controlling the gliding deceleration of the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/06
CPCG05D1/0676
Inventor 杨业黄万伟马卫华祁振强包为民郭涛吴浩梁禄扬徐国强刘毅
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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