Description
Test Techniques for Flight Control Systems of Large Transport Aircraft
Authors: Gao Yakui, An Gang, Zhi Chaoyou
Language: EnglishSubject for Test Techniques for Flight Control Systems of Large...:
Keywords
?Active control; Airborne software; Airborne systems; Aircraft conceptual design; Aircraft principle; Aircraft system; Airworthiness verification; Civil aircraft; Combined test; Computer unit; Control law; Control load test; Coverage; Electromagnetic compatibility; Electromechanical actuator; Engineering simulator; Engineering verification; Evaluation test; Flight control subsystem; Flight control system; Flight test; Flight test interface; Flight test plan; Flight verification; Flying quality; Ground test; Heading control channel; High lift control system; Hydraulic actuator; Integration test; Iron bird; Lateral control channel; Longitudinal control channel; Margin test; Military aircraft; Onboard functional test; Passive control; Pilot control units; Polarity inspection; Requirements analysis; Software testing; Spring load mechanism; System airborne software; Test management system; Test outline; Test support equipment; Test techniques; Traceability; Unit development; Unit test; Validation; Vehicle management system; Verification; Verification test
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Add to cart the book of Gao Yakui, An Gang, Zhi Chaoyou720 p. · 19x23.3 cm · Paperback
Description
/li>Contents
/li>Readership
/li>Biography
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1. Introduction2. Equipment test and validation for flight control system3. Software test and validation for flight control system4. Flight control law and flying qualities evaluation5. Tests of flight control subsystem6. Integration and validation based on the ‘iron bird’7. Onboard-ground?aircraft?test of flight control system8. Flight-test of flight control system9. Airworthiness test and validation for flight control system10. Current status and prospects for flight control system test and validation
Professor An Gang has a long career in the technical research of flight control system design, simulation system design and system integration. His main research direction is flight control system design, simulation system design, system integration and test verification, etc. He has been awarded several prizes and honors, including 1 Second Prize, 1 Third Prize of Commission on Science, Technology, and Industry for National Defense (COSTIND); 3 Second Prizes, 2 Third Prizes of Aviation Industry Corporation of China, Ltd (AVIC); Second and Third Honors during the 10th Five-Year plan aviation science and technology research; Youth Science and Technology Prize in 1st Shaanxi Society of Aeronautics and Astronautics (SSAA); Outstanding Individual First Prize of detailed design drawings release and C-type article test, First Honor of prototype first flight in AVIC’s National Major Special Projects. He has participated in the compilation of the book One Hundred Academicians One Hundred Books Series - Aerospace Science and Materials Science, and has published more than 10 scientific and technological papers
Professor Zhi Chaoyou has been engaged in the research of flight control system test and test technology for a long time. His main research direction is large and complex system test and test t
- Presents flight control system integration tests and validation for large transport aircraft
- Includes the most advanced methods and technologies available
- Details the latest research and its applications
- Offers theoretical and practical guidance that engineers can use
- Considers the state-of-the-art and looks to the future of flight control system tests