Repository logo
Log In(current)
  1. Home
  2. Colleges & Schools
  3. Graduate School
  4. Masters Theses
  5. Use of the naval air test center manned flight simulator for handling qualities evaluation of F/A-18 digital flight control system degraded modes
Details

Use of the naval air test center manned flight simulator for handling qualities evaluation of F/A-18 digital flight control system degraded modes

Date Issued
May 1, 1993
Author(s)
Ashby, Jeffrey S.
Advisor(s)
Ralph D. Kimberlin
Permanent URI
https://trace.tennessee.edu/handle/20.500.14382/33176
Abstract

The F/A-18 aircraft incorporates a digital "fly-by-wire" flight control system with four channel redundancy. In the event of a like failure in three or more of these channels, some control function is lost, and the system automatically reverts to a degraded (back-up) mode of operation. Degraded flight control modes of the F/A-18 are designed to enable the pilot to safely exit the combat arena, return to base, and land. In 1988, an F/A-18 aircraft was lost after the flight controls degraded to a mode which had never been flight tested. Analysis of that mishap forced Navy testers to reevaluate the need to flight test severely degraded flight control modes, and raised the question of whether results obtained from simulator testing could be used in lieu of high risk airplane tests. This thesis compares degraded mode handling qualities of the F/A-18 Manned Flight Simulator (MFS) with those experienced in the actual aircraft during the approach and landing phases. The objective is to evaluate the accuracy of the simulator in predicting degraded mode handling qualities and to provide future testers with recommendations on conduct of handling qualities testing in the simulator. Results show that the MFS could be used to predict aircraft degraded flight control mode handling qualities, provided that the test engineer and test pilot understand and manage simulator characteristics, pilot aggressiveness and proficiency. Incorporation of motion cueing into the MFS would probably enhance the accuracy of simulator test results. The simulator was not accurate in predicting Pilot Induced Oscillation (PIG) tendency, and in particular, did not predict the tendency for lateral PIG during landing approach seen in actual flight test. Test pilots and engineers should continually be alert for the potential of dangerous PIG which may not be predicted due to subtle differences between the simulator and airplane.

Degree
Master of Science
Major
Aviation Systems
File(s)
Thumbnail Image
Name

Thesis93A832.pdf

Size

2.27 MB

Format

Unknown

Checksum (MD5)

4afc734d8f9f848a3ba51583085bdc5a


University Libraries

1015 Volunteer Boulevard
Knoxville, TN 37996
865-974-4351

Map & Directions
Donate to the Libraries
  • About
  • John C. Hodges Society
  • Speaking Volumes magazine
  • Outreach
  • Directory
  • Employment
  • Policies
  • Library Intranet
University of Tennessee power T logo

The University of Tennessee, Knoxville
Knoxville, Tennessee 37996
865-974-1000

Events
A-Z
Apply
Privacy
Map
Directory
Give to UT
Accessibility

Built with DSpace-CRIS software - Extension maintained and optimized by 4Science