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Information Journal Paper

Title

UAV SIMULATION AND AUTOPILOT DESIGN WITH SILS & HILS

Pages

  33-36

Abstract

 In this article, the trend of UAV design using the AerSim software is first described then, different design steps of the autopilot program and the algorithms control tests using software -in-the-loop test in used for choosing the best control methods. In the next step, using the hardware-in-the-loop test, the auto-pilot program is validated. Finally, the flight test results & a real UAV is presented for comparison purpose. Sinse this control algorithm has been designed for a non-linear model aircraft considering the atmospheric noise, the results match well will real data and thus cause considerable decrease in real life tests.

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  • Cite

    APA: Copy

    LANGARI, M., SOLEIMANY, H., MIR MOHAMMAD SADEGHI, Y., & SABERI, M.T.. (2009). UAV SIMULATION AND AUTOPILOT DESIGN WITH SILS & HILS. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, 2(3), 33-36. SID. https://sid.ir/paper/199487/en

    Vancouver: Copy

    LANGARI M., SOLEIMANY H., MIR MOHAMMAD SADEGHI Y., SABERI M.T.. UAV SIMULATION AND AUTOPILOT DESIGN WITH SILS & HILS. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH[Internet]. 2009;2(3):33-36. Available from: https://sid.ir/paper/199487/en

    IEEE: Copy

    M. LANGARI, H. SOLEIMANY, Y. MIR MOHAMMAD SADEGHI, and M.T. SABERI, “UAV SIMULATION AND AUTOPILOT DESIGN WITH SILS & HILS,” JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, vol. 2, no. 3, pp. 33–36, 2009, [Online]. Available: https://sid.ir/paper/199487/en

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