Accession Number:

AD0767590

Title:

Control Configured Vehicle Ride Control System (CCV RCS). B-52 Control System Analysis, Synthesis, and Design.

Descriptive Note:

Technical rept. Dec 71-31 Jan 73,

Corporate Author:

AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1973-07-01

Pagination or Media Count:

221.0

Abstract:

The Control Configured Vehicle Ride Control System Program was conducted to demonstrate the capability of significantly improving the ride quality of a large flexible airplane and lengthening its structural life. The ride control system employs both horizontal and vertical canards to be installed and flight tested on the B-52 LAMS vehicle. The analysis, design, and flight demonstration of the ride control system was directed toward one discrete flight condition, low level, high speed. The ride control system was designed to reduce pilot station acceleration while flying through atmospheric turbulence. Author

Subject Categories:

  • Bombers

Distribution Statement:

APPROVED FOR PUBLIC RELEASE