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)
Initial Alignment and Augmentation of the ARINC 705 Strapdown AHRS LTR-81
1984
14 pages
Report
Keine Angabe
Englisch
Europäisches Patentamt | 2019
|AHRS AHRS flight control device based on mobile platform
Europäisches Patentamt | 2019
|AHRS AHRS flight control device based on mobile platform
Europäisches Patentamt | 2019