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題 名 | 飛彈實體模擬時尋標器與轉臺的轉動軸心不共點問題之探討=The Research on Different Rotation Centers between the Seeker and the Flight Table in Missile Hardware-in-the-loop Simulations |
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作 者 | 林義貴; | 書刊名 | 新新科技年刊 |
卷 期 | 12 2016.01[民105.01] |
頁 次 | 頁113-120 |
分類號 | 595.95 |
關鍵詞 | 實體迴路模擬; 飛行模擬轉臺; 電波模擬; 人造視線率; Hardware-in-the-loop simulation; Flight table; RF simulation; Artificially generating line-of-sight rate; |
語 文 | 中文(Chinese) |
中文摘要 | 在飛彈實體迴路模擬時,實務上因硬體機構的限制或其它因素,當尋標器被裝載在飛行模擬轉台上,常會出現兩者的轉動軸心不共點的情形,造成轉台在轉動時會帶動尋標器在空間中做小幅移動,尤其在離目標信號源的距離較短時,使得其準向誤差信號產生誤差。本文除做成因解說外,並做不同狀況的模擬,嘗試在定量上評估其影響,並以人造視線率模擬做法為例,提出相關改進的方法,以供日後有此需求時之參考。 |
英文摘要 | This paper presents when the seeker is not mounted at the center of rotation of the flight table due to the limits of the mechanical structure or other reasons in missile hardware-in-the- loop simulations. Erroneous boresight errors may be created when the flight table rotates, especially for the case of the short distance between the seeker and RF target source. It also presents an explanation depicting the reasons physically. And different conditions of simulations were performed in order to try to make some evaluations quantitatively. The compensations on artificially generating line-of-sight-rate simulations were proposed. It is hoped that these would be helpful in missile hardware-in-the-loop simulations in the future. |
本系統中英文摘要資訊取自各篇刊載內容。