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Microwave measurement and communication system and method for rendezvous and docking

A technology of microwave measurement and rendezvous and docking, which is applied to radio wave measurement systems, measurement devices, and the use of re-radiation, etc., can solve problems such as large weight and power consumption, fewer measurement and communication channels, and unavailable GPS measurement channels, etc., to achieve improvement Effect of Angle Measurement Accuracy

Active Publication Date: 2013-10-16
XIAN INSTITUE OF SPACE RADIO TECH
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

In lunar orbit rendezvous and docking, microwave radar is the core sensor and communication equipment for medium and long-range measurements. In lunar orbit rendezvous and docking, GPS measurement channels are no longer available, and there are few available measurement and communication channels, and there is a high demand for lightweight , the shortcomings of existing microwave measurement systems for rendezvous and docking are: the weight and power consumption are too large when integrating multiple functions using the traditional system, and the multi-functional system configuration and processing methods are difficult to solve high measurement accuracy and wide coverage , the contradiction between multifunctional integration and product lightweight, resulting in the limitations of the application of these methods

Method used

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  • Microwave measurement and communication system and method for rendezvous and docking

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Embodiment

[0048] The carrier frequency between the target aircraft and the tracking aircraft is selected from two frequency points in the Ka frequency band greater than 30GHz as the forward and reverse carrier waves. The information frame length is 200ms and QPSK modulation is used. One of the branches is designed as a measurement information frame. Its orthogonal branches are designed as communication information frames, and the pseudo-code rate is 10.23Mcps. In the host antenna array, the beam width of the main transceiver antenna is designed to be ±5 degrees, the angle measuring antenna is designed to be ±15 degrees, the primary capture antenna is designed to be ±20 degrees, the controllable antenna rotation angle of the host is greater than 120 degrees, and the auxiliary antenna is 120 degrees cone Wide-angle beam antenna; the transmission power of the main unit is 0.2W, and the transmission power of the auxiliary unit is 1W.

[0049] From the realization performance of the equipmen...

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Abstract

The invention discloses a microwave measurement and communication system for rendezvous and docking. The system comprises a main unit and an auxiliary unit, wherein the main unit is arranged on a tracking aircraft; the auxiliary unit is arranged on a target aircraft; the main unit comprises a main unit frequency source, a main unit signal processor, a main unit modulation transmitting channel, a main unit receiving channel, an angle measurement receiving channel, a main unit duplex coupler and a main unit antenna array; and the auxiliary unit comprises an auxiliary unit frequency source, an auxiliary unit signal processor, an auxiliary unit modulation transmitting channel, an auxiliary unit receiving channel, an auxiliary unit duplex coupler and an auxiliary unit antenna. Meanwhile, the invention also provides a microwave measurement and communication method for the rendezvous and docking employing the device. By the invention, under the conditions of large dynamic distance range and wide viewing angle between the tracking aircraft and the target aircraft, the distance, speed and angle of the target aircraft are measured by the tracking aircraft, and data communication between thetracking aircraft and the target aircraft is realized.

Description

technical field [0001] The invention relates to a microwave measurement and communication system and method for rendezvous and docking. Background technique [0002] At present, the microwave measurement and communication of rendezvous and docking in foreign countries adopts the traditional system of microwave radar, and some of them have communication functions through time-sharing applications. my country has also developed microwave radar in the rendezvous and docking project between the manned spacecraft and Tiangong-1, but the distance measurement and speed measurement of these devices adopt the traditional response system. The technologies used for angle measurement include amplitude ratio monopulse tracking angle measurement and interferometer angle measurement, working in L, S, X, Ku and other frequency bands. Typical and representative, for example, the space shuttle developed by Hughes Corporation of the United States is used for rendezvous, docking and communicat...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S13/72
Inventor 钟兴旺王登峰郑先安尚社踪念科赵峰张文会严琪杨瑞强蔡春贵
Owner XIAN INSTITUE OF SPACE RADIO TECH
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