Vision-only aircraft flight control

Christophe De Wagter, Alison A. Proctor, Eric N. Johnson

Research output: Contribution to conferencePaperpeer-review

20 Scopus citations

Abstract

Simulation tests showed that vision-only aircraft flight control is effective, even with very few image analysis measurements and a simple glider model. Simulations showed that a 1/3 crosswind versus launch speed velocity ratio is the maximum the glider can handle, without losing track of the window. Should 10 feet/second winds be expected, the glider would have to fly at least 25 to 35 feet per second forward speed.

Original languageEnglish (US)
Pages8.B.2/1-8.B.2/11
StatePublished - Dec 2 2003
EventThe 22nd Digital Avionics Systems Conference - Proceedings - Indianapolis, IN, United States
Duration: Oct 12 2003Oct 16 2003

Other

OtherThe 22nd Digital Avionics Systems Conference - Proceedings
CountryUnited States
CityIndianapolis, IN
Period10/12/0310/16/03

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Electrical and Electronic Engineering

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