مشاهده مشخصات مقاله
Real-time Hardware-in-the-loop Test for a Small Upper Stage Embedded Control System
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نویسنده (ها) |
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Mehrdad Ghorbani
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Milad Pasand
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Alireza Ghasem Bayati
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Neda Baheri
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مربوط به کنفرانس |
سمپوزیوم بینالمللی سیستمها و فنآوریهای بیدرنگ و نهفته RTEST 2018 |
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چکیده |
In this paper, the development of a real-time hardware-in-the-loop (HIL) test for a spacecraft is investigated. The spacecraft mission is to transfer a satellite from 400km circular to 400-7000km elliptical orbit by a small upper stage. The main parts of the mission are de-tumbling, pointing, spin-up, and orbital transfer maneuvers. The developed HIL test aims at demonstrating the performance of the guidance, navigation, and control (GNC) algorithms, simulating the mission operation plan (MOP), completing the end-to-end hardware verification, and testing throughout the whole mission. In the presented framework, four modules are considered: 1) Onboard computer (OBC) and onboard hardware (OBH) module; 2) Onboard software (OBS) module; 3) Flight simulator (FS) module; 4) Logger and command computer (LCC) module. The GNC algorithms and MOP are programmed in the OBC while it communicates with a six degrees of freedom flight simulator, implemented in C# language in the visual studio environment, via CAN bus. The HIL test is performed while sensors have been substituted with dummy thermal samples to simulate their energy consumption function, because the environmental conditions of space and the sensors dependence on the current attitude cannot be duplicated in the laboratory environment. The FS module can be executed in a real-time approach with the frequency of 1 kHz and even faster. All results have been proven to be satisfactory with respect to orbit transfer mission and consequently, the onboard hardware and software are verified to be reliable enough after several repeats of the test. |
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قیمت |
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برای اعضای سایت : ۱٠٠,٠٠٠ ریال
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برای دانشجویان عضو انجمن : ۲٠,٠٠٠ ریال
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برای اعضای عادی انجمن : ۴٠,٠٠٠ ریال
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خرید مقاله
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