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Integration simulation test method of space optical remote sensor

A technology of space optical remote sensing and simulation testing, which is applied in electrical testing/monitoring, instruments, radio wave measurement systems, etc. It can solve the problems of less coverage test functions, no comprehensive analysis and judgment ability, and poor performance, so as to avoid one-sided conclusions, The effect of solving real-time integrated detection technology problems and shortening the development cycle

Inactive Publication Date: 2010-05-12
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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Problems solved by technology

With the rapid development of space optical remote sensor technology, these devices have fewer coverage test functions, which are limited to some subsystem tests, and there are still shortcomings such as incomplete functions, poor performance, low precision, and no comprehensive analysis and judgment capabilities. It has been far from meeting the requirements of space optical remote sensor testing, and cannot undertake the task of automatic ground comprehensive testing of space optical remote sensors, which has brought difficulties to the development of space optical remote sensors

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  • Integration simulation test method of space optical remote sensor
  • Integration simulation test method of space optical remote sensor
  • Integration simulation test method of space optical remote sensor

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Embodiment Construction

[0024] The present invention is described in detail below in conjunction with examples, so that the purpose, characteristics and advantages of the present invention can be understood more deeply.

[0025] refer to figure 2 , the basic structure of the space optical remote sensor 6 is composed of 7 subsystems. The main body of the space optical remote sensor 8 includes mechanical structures such as lens barrels and supports. The optical subsystem 9 includes multiple optical lenses. CCD (Charge Coupled Device) The subsystem 10 includes a plurality of CCD chips, a CCD control circuit, a CCD data acquisition and processing circuit, an image transmission circuit communicating with the aircraft control system, and a communication circuit with the main control subsystem. The main control subsystem 11 includes a signal control circuit, a communication circuit with the aircraft control system, and a communication circuit with the CCD subsystem. The focusing subsystem 12 includes a foc...

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Abstract

An integration simulation test method of space optical remote sensor belongs to integration simulation test technology. A comprehensive simulation test system composed of a comprehensive analyzing and processing device, a special simulation test device, an auxiliary simulation test device and a synchronous clock device is connected on a tested space optical remote sensor to realize real-time parallel integration closed loop simulation test. Under the reference of unitary time provided by the synchronous clock device, first the special simulation test device simulates the work of a space aircraft, or key parts, units or special functions of the space optical remote sensor, collects state, data and signals of the space optical remote sensor, and transmits to the comprehensive analyzing and processing device; then the comprehensive analyzing and processing device transmits the analyzing result to the auxiliary simulation test device in real time to be displayed, printed and transmitted to the special simulation test device in real time so as to form a closed loop simulation test, thus achieving the aims of predicting, judging and appraising the space optical remote sensor rapidly on the ground.

Description

technical field [0001] The invention belongs to the field of industrial automation and relates to an integrated simulation test technology for space optical remote sensors. Background technique [0002] The space optical remote sensor is the core equipment of the space vehicle. The control system of the space vehicle issues commands and control parameters to the space optical remote sensor, and controls the optical imaging system to complete the imaging task of the ground scene, such as figure 2 shown. Usually, space optical remote sensors have to go through many comprehensive tests such as desktop joint test, electrical test, various environmental test and electromagnetic compatibility test from the development of the initial sample to the launch of the real sample. Generally, it needs to go through five stages: program demonstration, design, initial sample development, positive sample development and flight test. In addition to the program demonstration, it is necessary ...

Claims

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Application Information

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IPC IPC(8): G01S7/497G05B23/02
Inventor 胡君曹小涛王栋吴伟平徐抒岩
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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