Accession Number:

ADA350351

Title:

An In-Flight Investigation of Pilot-Induced Oscillation Suppression Filters During the Fighter Approach and Landing Task.

Descriptive Note:

Final rept. Jun 81-Oct 82,

Corporate Author:

ARVIN/CALSPAN CORP BUFFALO NY

Personal Author(s):

Report Date:

1981-10-01

Pagination or Media Count:

145.0

Abstract:

An investigation of pilot-induced oscillation suppress ion PIOS filters was performed using the USAFFlight Dynamics Laboratory variable stability NT-33 aircraft, modified and operated by Calspan. This program examined the effects of PIOS filtering on the longitudinal flying qualities of fighter aircraft during the visual approach and landing task. Forty evaluations were flown to test the effects of different PIOS filters. Although detailed analyses have not been undertaken, the results indicate that PIOS filtering can improve the flying qualities of an otherwise unacceptable aircraft configuration Level 3 flying qualities. However, the ability of the filters to suppress pilot-induced oscillations appears to be dependent upon the aircraft configuration characteristics. Further, the data show that the filters can adversely affect landing flying qualities if improperly designed. The data provides an excellent foundation from which detail analyses can be performed.

Subject Categories:

  • Military Aircraft Operations
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE