NASA NTRS · 19850006527
Closing the design loop on HiMAT (highly maneuverable aircraft technology)
Abstract
The design methodology used in the HiMAT program and the wind tunnel development activities are discussed. Selected results from the flight test program are presented and the strengths and weaknesses of testing advanced technology vehicles using the RPV concept is examined. The role of simulation on the development of digital flight control systems and in RPV's in particular is emphasized.
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Putnam, T. W., Robinson, M. R.. 1984-12-01. Closing the design loop on HiMAT (highly maneuverable aircraft technology). https://ntrs.nasa.gov/citations/19850006527
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