A gliding aircraft three-dimensional reentry guidance method based on analytical prediction

A technology of re-entry guidance and aircraft, applied in the field of three-dimensional re-entry guidance of gliding aircraft, which can solve problems such as difficult guidance, limited guidance methods of gliding aircraft, and limited maneuverability of gliding aircraft

Active Publication Date: 2019-05-10
NAT UNIV OF DEFENSE TECH
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AI Technical Summary

Problems solved by technology

However, there is a deficiency in these technical solutions: the angle of attack scheme generally needs to be given in advance based on the longitudinal range requirements, and only depends on adjusting the roll angle to take into account the lateral maneuvering requirements of the gliding aircraft
As a key control parameter to determine the maneuverability

Method used

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  • A gliding aircraft three-dimensional reentry guidance method based on analytical prediction
  • A gliding aircraft three-dimensional reentry guidance method based on analytical prediction
  • A gliding aircraft three-dimensional reentry guidance method based on analytical prediction

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Embodiment Construction

[0072] Such as figure 1 As shown, the implementation steps of the three-dimensional re-entry guidance method for gliding aircraft based on analytical prediction in this embodiment include:

[0073] 1) Considering the constraints of heat flux, overload, and dynamic pressure, as well as the constraints of angle of attack and roll angle during the flight of the gliding vehicle, construct a three-dimensional flight corridor with longitudinal lift-to-drag ratio, lateral lift-to-drag ratio, and energy as the frame ;

[0074] 2) Design the flight profile directly in the three-dimensional flight corridor based on the prediction model of the gliding vehicle motion, the flight profile includes the longitudinal lift-to-drag ratio-energy profile LD 1 (E) and lateral lift-to-drag ratio-energy profile LD 2 (E);

[0075] 3) Design a reasonable tilting and flipping strategy, namely:

[0076]According to whether the terminal handover point of the gliding aircraft has an entry angle requiremen

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Abstract

The invention discloses a gliding aircraft three-dimensional reentry guidance method based on analytical prediction. The method comprises the following implementation steps of: constructing a three-dimensional flight corridor taking a longitudinal lift-drag ratio, a lateral lift-drag ratio and energy as a standard frame by considering constraint conditions, directly designing a flight profile in the three-dimensional flight corridor based on a prediction model, designing a reasonable heeling overturning strategy, updating the flight profile, and tracking the flight profile to generate a heeling angle instruction and an attack angle instruction. The method is based on a high-precision analysis model; the aircraft target accessibility and the lateral maneuvering task requirements are comprehensively considered; A flight profile and an overturning strategy are directly designed in a three-dimensional flight corridor constructed by considering a plurality of constraint conditions; An attack angle instruction and a roll angle instruction are generated through profile tracking, so that the design of the three-dimensional reentry guidance method is completed, the integrity of dynamic information can be ensured, and the task adaptive capacity of the gliding aircraft under the long-distance large-range maneuvering condition is fully exerted.

Description

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Claims

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Application Information

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Owner NAT UNIV OF DEFENSE TECH
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