In-flight Simulation Study of Decoupled Longitudinal Controls for the Approach and Landing of a STOL Aircraft
Author: Benjamin Feinreich
Publisher:
Published: 1977
Total Pages: 84
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: Benjamin Feinreich
Publisher:
Published: 1977
Total Pages: 84
ISBN-13:
DOWNLOAD EBOOKAuthor: G. Kimball Miller
Publisher:
Published: 1974
Total Pages: 68
ISBN-13:
DOWNLOAD EBOOKA fixed-base visual simulation study has been conducted to evaluate the use of decoupled controls as a means for reducing pilot workload during approach and landing of an externally blown jet-flap short take-off and landing (STOL) transport. All six rigid-body degrees of freedom were employed with the aerodynamic characteristics based on wind-tunnel data. The primary piloting task was to use a flight director to capture and maintain a two-segment glide slope, with a closed-circuit television display of a STOL airport used during simulations of the flare and landing. The decoupled longitudinal controls used constant prefilter and feedback gains to provide steady-state decoupling of flight-path angle, pitch angle, and forward velocity. The pilots were enthusiastic about the decoupled longitudinal controls but believed the decoupled concept offered no significant advantage over conventional controls in the lateral mode.
Author: G. Kimball Miller
Publisher:
Published: 1975
Total Pages: 84
ISBN-13:
DOWNLOAD EBOOKAuthor: G. Kimball Miller
Publisher:
Published: 1979
Total Pages: 76
ISBN-13:
DOWNLOAD EBOOKAuthor: G. K. Miller (Jr)
Publisher:
Published: 1979
Total Pages: 76
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration
Publisher:
Published: 1978
Total Pages: 500
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published:
Total Pages: 1388
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1976
Total Pages: 1408
ISBN-13:
DOWNLOAD EBOOK