Engineering topics

Mosser, M. A.

Publications and source records attributed to Mosser, M. A..

3 records

NASA NTRS1982

Data acquisition/reduction system for flight testing general aviation aircraft

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.

Rummer, D. I.↗

NASA NTRS1982

A microcomputer-based system for noise characteristics analysis

A description is given of the design and use of a microcomputer-based system for the analysis and prediction of interior noise levels in general aviation aircraft constructed from novel materials. The system consists of a test chamber divided into two parts by a panel which has been fabricated from the material or combination of materials to be tested. A noise generator applies noise to one side of the specimen, while the microcomputer system measures and records the noise spectra on both sides of the specimen, so that its attenuation properties may be calculated and displayed by both a color CRT and X-Y plotter hard copy.

Mosser, M. A.↗

NASA NTRS1981

Development of a simple, self-contained flight test data acquisition system

This paper describes a simple, self-contained flight test data acquisition system. The system makes use of the latest sensor and microprocessor technology available, to reduce overall system costs. Coupled with this is the use of modern control theory techniques allowing minimization of data requirements, as well as flight time requirements. Capability of the system includes primarily stability and performance analysis of general aviation airplanes, although system versatility has been designed into the package. Presented are details of the prototype system constructed, as well as details of the data reduction technique utilized. Preliminary results of the flight test program have also been included which demonstrate the capability of this system.

Renz, R. R. L.↗