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飛行控制系統的自愈合控制 版權信息
- ISBN：9787121331718
- 條形碼：9787121331718 ; 978-7-121-33171-8
- 裝幀：一般膠版紙
- 冊數：暫無
- 重量：暫無
- 所屬分類：>
飛行控制系統的自愈合控制 本書特色
本書主要介紹自愈合控制概念的起源與研究現狀，著重描述飛行控制系統的自愈合控制的新方法。針對三自由度雙旋翼直升機，以狀態觀測器技術為基礎研究了三自由度雙旋翼直升機在發生執行器故障時的故障診斷方法，為自愈合控制策略設計提供準確的故障診斷結果；針對發生驅動器故障的四旋翼直升機，基于自適應控制理論，介紹了三種針對四旋翼直升機的自愈合控制方法；針對飛行器發生多故障情形，介紹了三種多故障自愈合控制設計方法。數字仿真及半物理仿真結果表明，這些研究結果可增強機載控制自愈合性，從而保證航空器在故障和損傷等惡劣條件下的安全飛行。
飛行控制系統的自愈合控制 內容簡介
本書主要介紹了雙旋翼直升機、四旋翼直升機、高超聲速飛行器的故障診斷與方法及自愈合控制方法。第1章作為緒論簡單介紹了自愈合控制技術的發展概況 ; 第2、3章研究了基于觀測器設計的雙旋翼直升機故障診斷方法及多故障下的自愈合控制方法 ; 第4-9章針對四旋翼直升機介紹了基于前饋補償、魯棒反步滑模等自愈合控制方法, 第10章討論了高超聲速飛行器的多故障魯棒自適應控制方法。
飛行控制系統的自愈合控制 目錄
第1 章 緒論 ················································································································ 1
1.1 自愈合控制的研究背景 ··························································································· 1
1.2 國內外研究現狀 ······································································································· 2
1.3 *新研究成果 ·········································································································· 6
第2 章 基于觀測器設計的雙旋翼直升機故障診斷方法 ····················································· 9
2.1 引言 ····················································································································· 9
2.2 雙旋翼直升機控制系統建模及半物理仿真平臺 ·················································· 10
2.2.1 縱列式雙旋翼直升機 ················································································· 10
2.2.2 雙旋翼直升機半物理仿真平臺·································································· 13
2.3 基于自適應觀測器的多執行器卡死故障診斷 ······················································ 22
2.3.1 執行器卡死故障系統描述 ········································································· 22
2.3.2 魯棒快速自適應故障估計方法·································································· 23
2.3.3 多模型故障診斷方法 ················································································· 26
2.3.4 仿真與分析 ································································································ 29
2.4 基于自適應滑模觀測器的執行器時變故障診斷 ·················································· 34
2.4.1 系統描述 ···································································································· 35
2.4.2 基于自適應滑模觀測器的故障診斷方法 ·················································· 36
2.4.3 仿真與分析 ································································································ 39
2.5 相對階大于1 的非線性系統執行器故障診斷 ······················································ 44
2.5.1 微分幾何基本知識 ····················································································· 44
2.5.2 三自由度雙旋翼直升機非線性模型分析 ·················································· 45
2.5.3 基于構造輔助輸出的執行器故障診斷 ······················································ 46
2.5.4 仿真分析 ···································································································· 50
2.6 本章小結 ················································································································ 53
第3 章 基于自適應控制的雙旋翼直升機多故障自愈合控制 ··········································· 54
3.1 引言 ····················································································································· 54
3.2 三自由度雙旋翼直升機改進模型 ········································································· 55
3.3 基于自適應控制的多故障自愈合控制器設計 ······················································ 58
3.4 仿真驗證及結果分析 ····························································································· 60
3.5 本章小結 ················································································································ 63
第4 章 含有未知參數的四旋翼直升機多故障自愈合控制 ··············································· 64
4.1 引言 ··················································································································· 64
4.2 四旋翼直升機動力學模型 ····················································································· 66
4.3 聯級控制系統基本控制器設計 ············································································· 67
4.4 針對執行器部分失效故障的滑模自愈合控制器設計 ·········································· 71
4.5 針對未知參數的自適應容錯控制器設計 ······························································ 75
4.6 各控制器間的時間尺度分析 ················································································· 77
4.7 仿真驗證及結果分析 ····························································································· 78
4.8 本章小結 ················································································································ 84
第5 章 基于前饋補償和直接自適應的四旋翼直升機自愈合控制 ··································· 85
5.1 引言 ···················································································································· 85
5.2 四旋翼直升機控制系統與
1.1 自愈合控制的研究背景 ··························································································· 1
1.2 國內外研究現狀 ······································································································· 2
1.3 *新研究成果 ·········································································································· 6
第2 章 基于觀測器設計的雙旋翼直升機故障診斷方法 ····················································· 9
2.1 引言 ····················································································································· 9
2.2 雙旋翼直升機控制系統建模及半物理仿真平臺 ·················································· 10
2.2.1 縱列式雙旋翼直升機 ················································································· 10
2.2.2 雙旋翼直升機半物理仿真平臺·································································· 13
2.3 基于自適應觀測器的多執行器卡死故障診斷 ······················································ 22
2.3.1 執行器卡死故障系統描述 ········································································· 22
2.3.2 魯棒快速自適應故障估計方法·································································· 23
2.3.3 多模型故障診斷方法 ················································································· 26
2.3.4 仿真與分析 ································································································ 29
2.4 基于自適應滑模觀測器的執行器時變故障診斷 ·················································· 34
2.4.1 系統描述 ···································································································· 35
2.4.2 基于自適應滑模觀測器的故障診斷方法 ·················································· 36
2.4.3 仿真與分析 ································································································ 39
2.5 相對階大于1 的非線性系統執行器故障診斷 ······················································ 44
2.5.1 微分幾何基本知識 ····················································································· 44
2.5.2 三自由度雙旋翼直升機非線性模型分析 ·················································· 45
2.5.3 基于構造輔助輸出的執行器故障診斷 ······················································ 46
2.5.4 仿真分析 ···································································································· 50
2.6 本章小結 ················································································································ 53
第3 章 基于自適應控制的雙旋翼直升機多故障自愈合控制 ··········································· 54
3.1 引言 ····················································································································· 54
3.2 三自由度雙旋翼直升機改進模型 ········································································· 55
3.3 基于自適應控制的多故障自愈合控制器設計 ······················································ 58
3.4 仿真驗證及結果分析 ····························································································· 60
3.5 本章小結 ················································································································ 63
第4 章 含有未知參數的四旋翼直升機多故障自愈合控制 ··············································· 64
4.1 引言 ··················································································································· 64
4.2 四旋翼直升機動力學模型 ····················································································· 66
4.3 聯級控制系統基本控制器設計 ············································································· 67
4.4 針對執行器部分失效故障的滑模自愈合控制器設計 ·········································· 71
4.5 針對未知參數的自適應容錯控制器設計 ······························································ 75
4.6 各控制器間的時間尺度分析 ················································································· 77
4.7 仿真驗證及結果分析 ····························································································· 78
4.8 本章小結 ················································································································ 84
第5 章 基于前饋補償和直接自適應的四旋翼直升機自愈合控制 ··································· 85
5.1 引言 ···················································································································· 85
5.2 四旋翼直升機控制系統與
展開全部
飛行控制系統的自愈合控制 作者簡介
陳復揚，江蘇揚州人，工學博士，教授，博士生導師。現為南京航空航天大學自動化學院黨委委員、自動控制系教工黨支部書記，長期從事自適應控制、故障診斷與容錯控制、自修復控制、自愈合控制、飛行控制、物聯網與控制技術、量子信息與控制理論、高鐵信息控制系統的故障診斷、道路交通管理控制等方面的科學研究。現為中國兵工學會自動控制專業委員會委員、江蘇省暨南京市航空航天學會自動控制專業委員會委員。近年來主持國家自然科學基金面上項目2項、航空科學基金1項；獲中國航空學會科學技術獎1項、出版專著3部、以第1作者發表學術論文60余篇( SCI收錄30篇)、申請發明專利20項。長期從事《自動控制原理》《自適應控制》《自適應控制與歌唱藝術》課程教學，主持校級教改項目6項、獲江蘇省教學成果二等獎1項、主編出版教材6部、發表教改論文10篇。
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