Accession Number:

ADA043526

Title:

Landing and Takeoff Roll-Out Augmentation.

Descriptive Note:

Final rept. Jan 72-Dec 74,

Corporate Author:

BENDIX CORP TETERBORO NJ FLIGHT SYSTEMS DIV

Personal Author(s):

Report Date:

1974-12-01

Pagination or Media Count:

32.0

Abstract:

The results of a computer study on four roll-out guidance control laws and a nosewheel steering configuration is included herein. Beam convergence, ground speed, and crosswind effects were included in the simulation. Author

Subject Categories:

  • Military Aircraft Operations

Distribution Statement:

APPROVED FOR PUBLIC RELEASE