pdf

Design and feasibility verification of embedded flight parameter sensing system

  • 2018-09-14
  • 268.16KB
  • Points it Requires : 2

The aerodynamic model of the embedded flight parameter sensing system (FADS) is briefly introduced, and the algorithm implementation of the system is described in detail using the X-33 aircraft of the United States as an example. The verification method of the FADS system is designed, and the verification results under another FADS system structure are listed. The results show that the calculation results of this flight parameter sensing system can meet the design requirements of the aircraft compared with the rigid results of the wind tunnel experiment.

unfold

You Might Like

Uploader
PKelect
 

Recommended ContentMore

Popular Components

Just Take a LookMore

EEWorld
subscription
account

EEWorld
service
account

Automotive
development
circle

About Us Customer Service Contact Information Datasheet Sitemap LatestNews


Room 1530, 15th Floor, Building B, No.18 Zhongguancun Street, Haidian District, Beijing, Postal Code: 100190 China Telephone: 008610 8235 0740

Copyright © 2005-2024 EEWORLD.com.cn, Inc. All rights reserved 京ICP证060456号 京ICP备10001474号-1 电信业务审批[2006]字第258号函 京公网安备 11010802033920号
×