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A lateral flight energy management method for unpowered aircraft

An energy management and aircraft technology, applied in non-electric variable control, instruments, three-dimensional position/channel control and other directions, can solve the problems of easy over-adjustment and complicated calculation process in the implementation process, improve combat effectiveness and avoid overshoot Large, easy-to-achieve effects

Active Publication Date: 2022-06-03
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the calculation process of the above method is relatively complicated, and it is easy to cause over-adjustment in the implementation process.

Method used

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  • A lateral flight energy management method for unpowered aircraft
  • A lateral flight energy management method for unpowered aircraft
  • A lateral flight energy management method for unpowered aircraft

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Embodiment Construction

[0040] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.

[0041] see figure 1 and figure 2 As shown, the embodiment of the present invention provides a lateral flight energy management method of an unpowered aircraft, which includes the steps of:

[0042] S1. According to the lateral position deviation and lateral speed deviation of the aircraft to the standard track, calculate the lateral deviation, and then obtain the cumulative direction through calculation; the cumulative direction represents the position deviation direction of the aircraft.

[0043] S2. Calculate the lateral speed guide amount according to the direction accumulation amount and the speed offset amount.

[0044] S3. Pass the above lateral position deviation through the inertial link and the proportional link to obtain the lateral position guidance amount.

[0045] S4. Perform a weighted summation of the lateral velocity guidan...

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Abstract

The invention discloses a lateral flight energy management method of an unpowered aircraft, which relates to the technical field of aircraft flight control. Obtain the cumulative amount of direction; the cumulative amount of direction indicates the position offset direction of the aircraft; calculate the lateral velocity guidance amount according to the cumulative amount of direction and speed offset; pass the lateral position deviation through the inertia link and the proportional link to obtain the lateral position guidance amount ; Carry out weighted summation of the lateral speed guidance amount and the lateral position guidance amount to generate a lateral guidance command to control the lateral flight of the unpowered aircraft. The present invention takes the standard track as the reference, comprehensively considers the lateral velocity deviation and the lateral position deviation, combines lateral guidance with speed control, dissipates excess fuel through lateral maneuvering, avoids over-adjustment, and realizes energy management of the aircraft.

Description

technical field [0001] The invention relates to the technical field of aircraft flight control, in particular to a lateral flight energy management method of an unpowered aircraft. Background technique [0002] When an unpowered aircraft performs long-distance and long-distance flight missions, the energy deviation caused by the deviation of aerodynamic parameters and atmospheric density will accumulate over time, eventually leading to excessive energy dispersion at the end, and even causing the trajectory to diverge during the flight. It is beneficial to the later task handover. Therefore, it is necessary to manage the energy of the aircraft, control the energy accumulation deviation, and prevent the trajectory from diverging. [0003] The energy of the aircraft is designed according to its maximum flight range. For general tasks, there will be a certain amount of energy surplus. Existing aircraft energy management methods are mainly to continuously predict the flight tra...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 朱正辉陈普华陈红艳田群方黄鑫鑫罗伟梁森李青付艺绮郭春霞
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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