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研究生:林港富
研究生(外文):Lin, Kang Fu
論文名稱:內模式適應性船舶自航器之設計
論文名稱(外文):An Internal Model Control Approach to the Design of Adaptive Ship Steering Autopilot
指導教授:曾慶耀曾慶耀引用關係
指導教授(外文):Lee Tai-Shen
學位類別:碩士
校院名稱:國立海洋大學
系所名稱:航運技術研究所
學門:運輸服務學門
學類:運輸管理學類
論文種類:學術論文
論文出版年:1998
畢業學年度:86
語文別:中文
論文頁數:80
中文關鍵詞:內模式控制適應性自航器遞迴式最小平方法參考信號調節法舵角飽和角速率限制
外文關鍵詞:Internal Model ControlAdaptive AutopilotRecursive Least-Squares MethodReference Conditioning TechniquesRudder SaturationSlew Rate Limitation
相關次數:
  • 被引用被引用:15
  • 點閱點閱:269
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摘要 本文結合內模式控制(Internal Model Control, IMC)及遞迴式最
小平方法來設計適應性航向控制器。內模式控制設計法具有易於滿足系統
常態內部穩定(nominal internal stability)之特性。文中針對一二階
Nomoto船舶模式進行設計。依據內模式控制設計所得自航器為二階具PID
型態之控制器,所得控制器之增益常數直接與船舶模式參數,及決定系統
反應速度之設計參數有關。因此只要給定船舶特性常數,如舵效增益、時
間常數,則控制器參數可依據需求之系統反應規格決定之。由於船舶之特
性在不同船速、水域等之操作狀況下將有所不同,藉由遞迴式最小平方法
可找出同操作狀況下之船舶特性參數後,則自航器之增益常數隨即可定出
。對於舵機之飽和及速率限制等非線性現象,為了防止積分終結(
integrator windup)的情形產生,採用參考信號調節(reference signal
conditioning)的方法,以避免系統不穩定的現象產生。其原理在於修正
參考輸入訊號,使得控制器輸出控制指令與舵機實際可提供之控制能力一
致,如此則可確保系統充分發揮其應有功能而不致陷於舵機飽和及速率限
制之邊界而造成不穩定現象,此一穩定性需求之考慮在同時進行參數估測
及控制器參數設定之適應控制系統尤其重要。本文提出之適應性自航器設
計方法具有設計簡單、易於實現之特性,經由電腦模擬顯式示本文提出之
適應性自航器在不同水深狀況下之航向變換皆有滿意之控制效果。
Abstract-This paper is concerned with the design of an adaptive
ship steering autopilot. Specifically, an Internal Model
Control(IMC) design method is coupled with a recursive least-
squares method in forming the adaptive autopilot. The IMC design
method is very attractive from the viewpoint of its relative
easiness in satisfying the nominal internal stability
conditions. A second order Nomoto model is taken as the ship
model in the controller design. The autopilot obtained with the
IMC design method is equivaa 2nd order PID type controller.
Moreover, the proposed IMC design method offers explicit
formulas relating the autopilot gain coefficients to the ship
model parameters and a design parameter that determines the
speed of response of the system. A recursive least-squares
method is employed in estimating the ship model parameters under
various operating conditions, and then the autopilot gain
coefficients can be determined accordingly. This allows the
autopilot to adapt to changing operating conditions. To avoid
instability phenomenon caused by rudder saturation and rudder
rate limitation, a reference conditioning technique is employed
to bring the rudder limit and rudder rate limit into the
adaptation design consideration. Specifically, the reference
signal is modified such that the rudder input command is always
consistent with the actual rudder input supplied by the
actuator. That is, the controller uses the full power of the
steering machine whenever necessary, without pushing the
steering machine to the nonlinear saturation and slew rate
limitation boundaries indefinitely. This so-called anti-windup
consideration is really necessary, since the wind-up problem is
much serious in adaptive control than in standard controller
with constant gain. Computer simulations indicate that the
proposed adaptive autopilot achieves satisfactory course-
changing maneuvers while sailing through waters of different
depth.
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