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Determining method for terminal guidance shift-exchange conditions of reenter vehicle

A technology for re-entry aircraft and determination method, which is applied in the field of determining the terminal guidance shift conditions of re-entry aircraft, and achieves the effects of enhancing robustness, improving fault tolerance, and reducing command hardware limits

Active Publication Date: 2014-01-01
CHINA ACAD OF LAUNCH VEHICLE TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, it is a high-reliability, high-precision flight guidance control mode, which brings many new challenges and difficulties to the control system

Method used

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  • Determining method for terminal guidance shift-exchange conditions of reenter vehicle
  • Determining method for terminal guidance shift-exchange conditions of reenter vehicle
  • Determining method for terminal guidance shift-exchange conditions of reenter vehicle

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Embodiment Construction

[0026] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0027] Such as figure 1 As shown, the present invention relates to a method for determining the handover condition of the terminal guidance of a reentry vehicle, and the specific steps are as follows:

[0028] 1. Generate preset shift points;

[0029] Such as figure 2 As shown in , set the reentry constraint boundary (heat flow, overload, dynamic pressure, etc.) through the given reentry point information (including position, velocity, velocity inclination and attitude) and strike target information (target position, velocity), Through the simulation planning, the longitudinal profile of the re-entry vehicle is generated, and the preset handover point information that meets the flight requirements is initially obtained.

[0030] The planning of the reentry trajectory can adopt the commonly used reentry trajectory optimization algorithm based on the ...

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Abstract

The invention discloses a determining method for terminal guidance shift-exchange conditions of a reenter vehicle. The determining method includes (1), generating preset shift-exchange point information; (2), correcting the preset shift-exchange point information generated in step (1), and generating a preset shift-exchange point error ball; (3), designing guidance gain which is changeable with time; (4), determining a command smoothing time factor sequence sorted according to time; (5), determining shift-exchange logic, starting terminal guidance of a seeker when the shift-exchange logic is completely met; (6), in the process of midcourse guidance flight of the reenter vehicle, performing midcourse guidance by the aid of the guidance gain, which is changeable with the time, determined in step (3), judging whether the shift-exchange logic determined in step (5) is met or not in real time, starting the terminal guidance of the seeker when the shift-exchange logic is met, picking a factor from the command smoothing time factor sequence determined in step (4) according to order, performing smoothing on the midcourse guidance and the terminal guidance by the factor, performing guidance according to a command subjected to smoothing, and shifting to the simple terminal guidance of the seeker after preset time is reached.

Description

technical field [0001] The invention belongs to the technical field of weapon system design, and relates to a method for determining the shift condition of the terminal guidance of a reentry vehicle. The invention is mainly applied to the design and realization of the transition conditions of the middle and terminal guidance of the reentry precision strike aircraft, so as to ensure the strike precision of the payload. Background technique [0002] Reentry vehicles have the characteristics of high dynamics and multiple constraints, which are especially important for vehicles with terminal guidance capabilities. A reentry vehicle with terminal guidance capability needs to experience a wide range of speed changes and altitude changes, and the performance requirements for the guidance and control system are relatively strict. In general, different guidance systems are used for intermediate guidance and terminal guidance. After the mid-to-terminal guidance is handed over, the po...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41G3/00
Inventor 吴炜平李杰奇张振兴王炀刘刚张永蔡巧言张旭辉
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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