New architectures for UAV flight control avionics

Gidado Yisa Immanuel, Eric Johnson

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Scopus citations

Abstract

Commercial and military aircraft utilize proven data bus standards such as MIL-STD-1553B and ARINC 429. However, future avionics systems may take greater advantage of commercial hardware and networking technology. With the increased processors and speeds, it is possible to begin challenge the fundamental avionics architectures used for navigation and flight control. This is particularly true for UAVs, where there is currently rapid change. Goals of new architectures include reduced development time, cost; increased testability; lead to quicker flight validation, and higher integrality. Of these, the concepts addressed in a new architecture include scheduling tasks and continuous integration.

Original languageEnglish (US)
Title of host publicationAIAA/IEEE Digital Avionics Systems Conference - Proceedings
Volume2
Publication statusPublished - Jan 1 2002
EventAir Traffic Management for Commercial and Military Systems - Irvine, CA, United States
Duration: Oct 27 2002Oct 31 2002

Other

OtherAir Traffic Management for Commercial and Military Systems
CountryUnited States
CityIrvine, CA
Period10/27/0210/31/02

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All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Electrical and Electronic Engineering

Cite this

Immanuel, G. Y., & Johnson, E. (2002). New architectures for UAV flight control avionics. In AIAA/IEEE Digital Avionics Systems Conference - Proceedings (Vol. 2)