Initial Alignment and Augmentation of the ARINC 705 Strapdown AHRS LTR-81,

Abstract

After systems hardware description the attitude, heading and vertical loops are discussed. System simulation results are compared with flight test results achieved during A 300 B4 FFC flight certification and BMFT/LITEF sponsored flight tests. Techniques for further system improvements are shortly described. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1984
Accession Number
ADP003626

Entities

People

  • M. Kleinschmidt
  • W. Hassenpflug

Tags

DTIC Thesaurus Topics

  • Inertial Navigation Systems
  • Performance Tests
  • Simulations

Readers

  • Inertial Navigation Systems.
  • Software Engineering