Aerospace Control and Guidance Systems Committee

Announcements

You must first log in to access prior meeting presentations, register for a meeting, or nominate some for the Ward Award.

If you do not have a login account, or cannot remember the email address associated with your account, please click on the Application Form link below.

Login

Site Search

Search our site:

Upcoming Events

Photos

Meeting Highlights New!

Subcommittee S

Prior Meetings

Abstracts may be viewed by anyone. Presentations are only available to active members who have logged in.

Meeting 132
(coming soon)

Home

Ward Memorial Award

Planning Advisory Board

Downloads

Constitution and By-Laws

About

History

Contact Us

← Return to agenda

Meeting	ACGS Committee Meeting 113 - Englewood, Colorado - March 2014
Agenda Location	4 GENERAL COMMITTEE TECHNICAL SESSION 4.1 Government Agencies Summary Reports 4.1.1 DLR 4.1.1.1 DLR
Title	DLR
Presenter	Oliver Brieger
Available Downloads*	presentation
	Downloads are available to members who are logged in and either Active* or attended this meeting.
Abstract	DLR - Flight Experiments Fleet Overview and Recent Flight Research Projects Oliver Brieger Head of Flight Operations The presentation gives an overview of the most recent projects currently conducted on DLR flight research vehicles. The high altitude long endurance research aircraft HALO has attained ‘mission ready’ status with all the major modifications completed, the respective STCs granted and the first long range missions successfully completed. On one of the turboprop Dornier 228 a digital autoflight system will be developed and integrated, allowing advanced 4-D navigation and surrogate UAV applications. For the rotary wing in-flight simulator ACT/FHS new control laws for an automatic transition to hover are being developed and are to be tested in the second half of 2014. On DLR’s A320 testbed a test campaign is being prepared investigating nonlinear aerodynamics effects before, during and post stall for high lift configurations, measuring wing pressure distribution, wing deformation, flow transition and separation and facilitating airflow visualization by means of pressure belts, hot film, IR cameras and lasers. The gathered data will be used to enhance analytical methods to model aerodynamic effects in this extreme flight regime.