[[abstract]]本文提出三維空間導引律通式,並利用相位法在修正的極座標下成功的分析其相關之目標物捕捉條件。一般在導引律方面之論文皆需假設小量瞄準誤差,或其結果僅能適用於二維空間之情況,然本文所提方法則無此限制。本方法可直接推展至目標物逃逸,但無法得知其加速度時,其捕捉條件之分析。另外對系統可觀性亦做了所需充分條件之探討。[[abstract]]In this paper, we presents the general three-dimensional guidance law. With the aid of the modified polar coordinate, the expression of relative dynamics between target and missile becomes simple, and the constructed guidance law is intuitive and naive. Furthermore, a phase plane method is used to analyze the capture condition of the corresponding guidance law. The result is not restricted to time -invariant navigation constant. For a nonmaneuvering target or a maneuvering target but with known acceleration, it can be seen that only two of the state vectors are relat...
[[abstract]]本文主旨的探討純比例導引律對飛彈性能的影響, 經數值模擬分析結果可知在一般狀態下, 令導航係數為常數表現並不是很好, 例如在尾追時取導航係數值較大表現較好, 但在側擊時如取相同...
[[abstract]]Unlike the traditional ways adopted by most of the researchers, the rotating angle of re...
An approach to integrated guidance/autopilot design is considered in this study. It consists of two ...
[[abstract]]本文提出三維空間導引律通式,並利用相位法在修正的極座標下成功的分析其相關之目標物捕捉條件。一般在導引律方面之論文皆需假設小量瞄準誤差,或其結果僅能適用於二維空間之情況,然本文所...
[[abstract]]In this paper, we presents the general three-dimensional guidance laws. With the aid of ...
[[abstract]]In this paper, we presents the general three-dimensional guidance laws. With the aid of ...
[[abstract]]Since the proportional navigation guidance law was first introduced, many of the researc...
[[abstract]]A method is used to analyze the capture area of general 3D true proportional navigation ...
[[abstract]]Since the proportional navigation guidance law was first introduced, many of the researc...
[[abstract]]In this paper, a novel method is used to analyze the capture area of three-dimensional g...
[[abstract]]In this work, the capture region of the general ideal proportional navigation guidance l...
計畫編號:NSC100-2221-E032-005 研究期間:20110801~20120731 研究經費:413,000[[abstract]]In the past few decades, de...
© Institution of Mechanical Engineers.The true proportional navigation guidance law, the augmented p...
[[abstract]]本文旨就尋標器離軸角先天條件的限制, 而使用純比例導引律並配合保持離軸角(Off-borsight)為定值的方法(偏角追逐法), 來解決尋標器追蹤迴路無法穩定追蹤的困擾, 並探...
For several decades, guidance problems for interception have been extensively studied, and some guid...
[[abstract]]本文主旨的探討純比例導引律對飛彈性能的影響, 經數值模擬分析結果可知在一般狀態下, 令導航係數為常數表現並不是很好, 例如在尾追時取導航係數值較大表現較好, 但在側擊時如取相同...
[[abstract]]Unlike the traditional ways adopted by most of the researchers, the rotating angle of re...
An approach to integrated guidance/autopilot design is considered in this study. It consists of two ...
[[abstract]]本文提出三維空間導引律通式,並利用相位法在修正的極座標下成功的分析其相關之目標物捕捉條件。一般在導引律方面之論文皆需假設小量瞄準誤差,或其結果僅能適用於二維空間之情況,然本文所...
[[abstract]]In this paper, we presents the general three-dimensional guidance laws. With the aid of ...
[[abstract]]In this paper, we presents the general three-dimensional guidance laws. With the aid of ...
[[abstract]]Since the proportional navigation guidance law was first introduced, many of the researc...
[[abstract]]A method is used to analyze the capture area of general 3D true proportional navigation ...
[[abstract]]Since the proportional navigation guidance law was first introduced, many of the researc...
[[abstract]]In this paper, a novel method is used to analyze the capture area of three-dimensional g...
[[abstract]]In this work, the capture region of the general ideal proportional navigation guidance l...
計畫編號:NSC100-2221-E032-005 研究期間:20110801~20120731 研究經費:413,000[[abstract]]In the past few decades, de...
© Institution of Mechanical Engineers.The true proportional navigation guidance law, the augmented p...
[[abstract]]本文旨就尋標器離軸角先天條件的限制, 而使用純比例導引律並配合保持離軸角(Off-borsight)為定值的方法(偏角追逐法), 來解決尋標器追蹤迴路無法穩定追蹤的困擾, 並探...
For several decades, guidance problems for interception have been extensively studied, and some guid...
[[abstract]]本文主旨的探討純比例導引律對飛彈性能的影響, 經數值模擬分析結果可知在一般狀態下, 令導航係數為常數表現並不是很好, 例如在尾追時取導航係數值較大表現較好, 但在側擊時如取相同...
[[abstract]]Unlike the traditional ways adopted by most of the researchers, the rotating angle of re...
An approach to integrated guidance/autopilot design is considered in this study. It consists of two ...