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大型運輸機飛行控制系統試驗技術(英文版國際版)(精)/大飛機出版工程

  • 作者:高亞奎//安剛//支超有|責編:江璇//劉盼盼|總主編:顧誦芬
  • 出版社:上海交大
  • ISBN:9787313241313
  • 出版日期:2023/09/01
  • 裝幀:精裝
  • 頁數:699
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內容大鋼
    大型運輸機飛行控制系統是影響飛機安全、功能與性能的核心系統之一,對其進行科學、規範、合理、全面的試驗驗證是保證飛機成功研製的關鍵。本書詳細描述了飛行控制系統的機載設備試驗、控制律與飛行品質評估試驗、系統綜合試驗、「鐵鳥」集成試驗、機上地面試驗、結構模態耦合試驗、電磁兼容試驗和飛行試驗等。本書是作者多年理論研究成果和工程實踐的總結。內容新穎、系統性強、理論聯繫實際,具有較高的理論和工程應用價值。

作者介紹
高亞奎//安剛//支超有|責編:江璇//劉盼盼|總主編:顧誦芬

目錄
CHAPTER 1 Introduction
  1.1  Overview
  1.2  Current situation and development trend of flight control system testverification technologies
    1.2.1  Development of the verification test
    1.2.2  Current development of flight control system test verificationtechnologies
    1.2.3  Development trends of the verification test
  1.3  Features and evaluation management of a flight control systemverification test
    1.3.1  Basic features of a verification test
    1.3.2  Functions of a verification test
    1.3.3  Principles for verification test design
    1.3.4  Technical management of a verification test
  1.4  Requirements definition of flight control system verification
    1.4.1  Requirements definition
    1.4.2  Requirements verification and assignment
    1.4.3  Coverage and traceability
    1.4.4  Requirements management tools
    1.4.5  System verification supports aircraft-level verification
  1.5  Engineering practice of the flight control system test verification
  1.6  Flight control system test verification
    1.6.1  Introduction to the background aircraft flight control system
    1.6.2  Content of a verification test
    1.6.3  Procedures of a verification test
CHAPTER 2 Unit test of the flight control system
  2.1  Overview
    2.1.1  Basic process of unit development
    2.1.2  Categories of unit tests
    2.1.3  Basic principles for the selection of test items
    2.1.4  Classification of the flight control system unit
    2.1.5  Basis and requirements for the preparation of the unit test outline
  2.2  Basic functional/performance test
    2.2.1  General requirements of test
    2.2.2  Control and display unit
    2.2.3  Computer unit
    2.2.4  Manipulator unit
    2.2.5  Mechanical drive unit
    2.2.6  Mechanical transmission unit
    2.2.7  Mechanical actuating unit
    2.2.8  Sensor unit
  2.3  Strength and stiffness test
    2.3.1  Test objectives and test requirements
    2.3.2  Test items and test methods
    2.3.3  Judging criteria and results handling
  2.4  Power characteristic test
    2.4.1  Test items and reduction principles
    2.4.2  Test objectives and test requirements
    2.4.3  Test items and test methods
    2.4.4  Judging criteria and results handling
    2.4.5  Test example: Power characteristic test of flight control computer
  2.5  Dielectric strength test
    2.5.1  Test objectives and test requirements

    2.5.2  Test items and test methods
    2.5.3  Judging criteria and results handling
  2.6  Mechanical environment test
    2.6.1  Acceleration test
    2.6.2  Vibration test
    2.6.3  Noise test
    2.6.4  Shock test
  2.7  Natural environment test
    2.7.1  Low pressure (altitude) test
    2.7.2  High temperature test
    2.7.3  Low temperature test
……
CHAPTER 3 Verification and validation of flight control system airborne software
CHAPTER 4 Flight control system control law and the flying quality evaluation
CHAPTER 5 Combined test of the flight control subsystem
CHAPTER 6 Iron bird integration test of the flight control system
CHAPTER 7 Onboard ground test of the flight control system
CHAPTER 8 Flight test of the flight control system
CHAPTER 9 Airworthiness verification test of the flight control system
CHAPTER 10 Development and expectations on test techniques of the flight control system
INDEX

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