The development of a data acquisition/reduction system for use in the flight testing of general aviation aircraft is described. Design objectives for the system are adequate accuracy, ease of installation and removal from aircraft, simplicity of operation, and low cost. A 16-channel working system has been constructed, and tested in the collection of flight test data from a Cessna 172 aircraft, which uses as the basis of its design an AIM65 microcomputer. Data is reduced with a MINC minicomputer system. Attention is given to the onboard installation of computer, battery and transducer modules incorporated by the system.
Data acquisition/reduction system for flight testing general aviation aircraft
Mini and microcomputers in control and measurement; International Symposium ; 1981 ; San Francisco, CA
1982-01-01
Miscellaneous
No indication
English
Flight data recording in aircraft of general aviation
Tema Archive | 1998
|General Aviation Aircraft Empennage Flight Loads
SAE Technical Papers | 1999
|General Aviation Aircraft Empennage Flight Loads
British Library Conference Proceedings | 1999
|Flight Data Collection for General Aviation Aircraft Simulation Validation
British Library Conference Proceedings | 2009
|