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Development of a simple, self-contained flight test data acquisition system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rummer, D. I. Roskam, J. Clarke, R. Shane, D. |
| Copyright Year | 1982 |
| Description | The flight test system described combines state-of-the-art microprocessor technology and high accuracy instrumentation with parameter identification technology which minimize data and flight time requirements. The system was designed to avoid permanent modifications of the test airplane and allow quick installation. It is capable of longitudinal and lateral-directional stability and control derivative estimation. Details of this system, calibration and flight test procedures, and the results of the Cessna 172 flight test program are presented. The system proved easy to install, simple to operate, and capable of accurate estimation of stability and control parameters in the Cessna 172 flight tests. |
| File Size | 16293126 |
| Page Count | 243 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820015371 |
| Archival Resource Key | ark:/13960/t5m95230x |
| Language | English |
| Publisher Date | 1982-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Instrumentation Accelerometers Flight Tests Attitude Control Data Acquisition Airborne/spaceborne Computers Data Processing Aerodynamic Stability Parameterization Computer Programs Equipment Specifications Cessna 172 Aircraft Attitude Stability Microprocessors Computer Techniques Gyroscopes Onboard Equipment Flight Time Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
