頁籤選單縮合
題名 | 飛行追蹤控制系統之穩定性、可觀察性及可控制性分析=Stability, Observability and Controllability Analysis of Flight Tracking Control System |
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作者 | 張松國; | 書刊名 | 華岡工程學報 |
卷期 | 13 1999.06[民88.06] |
頁次 | 頁61-70 |
分類號 | 447.85 |
關鍵詞 | 飛行追蹤控制系統; Nonlinear flight control; Stability; Controllability; Observability; |
語文 | 中文(Chinese) |
中文摘要 | 飛行追蹤控制系統的任務在精確地追蹤導航命令,使追蹤誤差降至最小。而飛彈 使用傾斜轉彎控制策略可降低側滑角,消除誘導側滾力距,且提高氣動力性能。作者前曾提 出非線性飛彈動力學模式及多項式迴授控制策略以達成精確的追蹤控制。而本文將對此非線 性控制系統之穩定性、可觀察性及可控制性加以進一步之分析。 |
英文摘要 | It is well known that bank to turn steering is more attractive in missile performance over skid to turn steering. Author (Chang 1990) derived a nonlinear missile dynamic model of six degree of freedom and proposed an optimal nonlinear tracking control method to solve this problem. In this paper author applies some theories to discuss the stability of the optimal nonlinear control method. The controllability and observability of this nonlinear flight tracking control system are also discussed. |
本系統之摘要資訊系依該期刊論文摘要之資訊為主。