The integrated system for design, analysis, system simulation and evaluation of the small satellite

Sun, Zhiyong; Xu, Guodong; Lin, Xiaohui; Cao, Xi‐Ren

doi:10.1016/s0965-9978(00)00055-7

Cited by 6 publications

(2 citation statements)

References 5 publications

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“…[6] The simulator can generate the ground data, the bus data and the telemetry downlink data and receive the remote commands from ground and simulate the instruction executing process. Fig.2 The integrated electronic simulator connects with the attitude and orbit control system (AOCS) and the ground overall checkout equipment through the net with the TCP/IP protocol.…”

Section: Research On Digital Simulation Of Satellite Integrated Electmentioning

confidence: 99%

Research on digital simulation of satellite integrated electronic system

2014

11th IEEE International Conference on Control &Amp; Automation (ICCA)

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Satellite simulation technology is an effective method to reduce the risk of satellite system application and the production cost. With the satellite electronic system tending to integration and comprehension, it is particularly necessary to do researches on simulation of the satellite integrated electronic system (IES). The paper explains the design ideology of IES digital simulation, builds a simulation framework, introduces the realization of the digital simulation of IES, and develops universal and authentic simulation software. In simulation application level, the paper realizes the function of the real satellite IES and the software has been applied to real satellite testing system.

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Section: Research On Digital Simulation Of Satellite Integrated Electmentioning

confidence: 99%

Research on digital simulation of satellite integrated electronic system

2014

11th IEEE International Conference on Control &Amp; Automation (ICCA)

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“…The modern small satellite and its ground application system adopts modern new and high technologies to enhance greatly the "function density" of satellite and employ new design concepts and scientific management methods, so that the modern small satellites and its ground application system have many remarkable characteristics such as low cost, light weight, small size, high performance, short development period, flexible launching and convenient application, etc. [1,2] .…”

Section: Introductionmentioning

confidence: 99%

Transmission-type stereo mapping micro-satellite payload and ground application system

et al. 2005

International Conference on Space Information Technology

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With the development of modern small satellite technology, it is potential and significant to use the new technology for the earth observation. The stereo mapping micro-satellite-"Experiment Satellite 1", designed and built by Harbin Institute of Technology, is taken as an example for discussion of the relevant technologies and corresponding principle of the satellite payload and its ground application system. The ground application system receives the stereo photographs data from the "Experiment Satellite 1" and then produces surveying products such as digital elevation map, digital orthoimage and digital topographic map, etc. "Experiment Satellite 1" is the first satellite where three-line-array CCD camera is used triumphantly in world for stereo mapping. It will have profound influence on the earth observation technique.

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Sensor fault estimation and compensation for microsatellite attitude control systems

Gao

Jiang

Shi

et al. 2010

Int. J. Control Autom. Syst.

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In this paper, the problem of sensor fault estimation and compensation for microsatellite attitude dynamics is investigated by using a descriptor system approach. Firstly, a linear model of microsatellite attitude dynamics is given. Based on the proposed linear microsatellite attitude dynamics, an augmented descriptor system is constructed by letting the sensor fault term be an auxiliary state vector. Using linear matrix inequality approach, a state-space observer is designed for the augmented descriptor microsatellite attitude dynamics, which can estimate microsatellite attitude dynamics state vector and sensor fault simultaneously. In terms of the estimated sensor fault information, sensor fault compensation is also performed. Finally, a simulation example is given to illustrate the effectiveness and potential of the proposed techniques.

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The integrated system for design, analysis, system simulation and evaluation of the small satellite

Cited by 6 publications

References 5 publications

Research on digital simulation of satellite integrated electronic system

Research on digital simulation of satellite integrated electronic system

Transmission-type stereo mapping micro-satellite payload and ground application system

Sensor fault estimation and compensation for microsatellite attitude control systems

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