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

 

E-mail: 

 

Password: 


Forgot your password?

Application Form


 

Site Search

Search our site:
 
 

Upcoming Events


Register for Meeting 132
(please log in first)

 
 

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)

Meeting 131

Meeting 130

Meeting 129

Meeting 128

Meeting 127

Meeting 126

Meeting 125

Meeting 124

Meeting 123

Meeting 122

Meeting 121

Meeting 120

Meeting 119

Meeting 118

Meeting 117

Meeting 116

Meeting 115

Meeting 114

Meeting 113

Meeting 112

Meeting 111

Meeting 110

Meeting 109

Meeting 108

Meeting 107

Meeting 106

Meeting 105

Meeting 104

Meeting 103

Meeting 102

Meeting 101

Meeting 100

Meeting 99

Meeting 98

Meeting 97

Meeting 96

Meeting 95

Meeting 94

Meeting 93

Meeting 92

 
HomeWard Memorial AwardPlanning Advisory BoardDownloadsConstitution and By-LawsAboutHistoryContact Us

  ← Return to agenda

MeetingACGS Committee Meeting 110 - Auburn, Maine - October 2012
Agenda Location4 GENERAL COMMITTEE TECHNICAL SESSION
4.2 Government Agencies Summary Reports
4.2.3 DLR
4.2.3.0 DLR
TitleDLR
PresenterKlause-Uwe Hahn
Available Downloads*presentation
*Downloads are available to members who are logged in and either Active or attended this meeting.
AbstractGoodbye ATTAS -
- retirement of an outstanding flying testbed

DLR’s flying testbed officially retired on June 27th 2012 after a service period of about 27 years. The basic aircraft is a VFW 614 manufactured by the United Aeronautical Factories of Bremen. It is a twin engine short range aircraft where the engines are unusually mounted on top of the wings. The first VWF 614 made its maiden flight in 1971. The serial number of ATTAS is G17 out of 19 aircraft built. Thirteen of the manufactured aircraft went into service before the VFW 614 program was stopped in 1977. The G17 went into service at DLR on October 24th 1985 after a modification period which started in 1982. During this period the aircraft was equipped with Direct Lift Control Flaps (providing a 5 DoF In Flight capability), an experimental duplex electro-optical Fly-by-Wire system, numerous sensors, data acquisition and recording devices and an online basic and experimental data monitoring system. The safety concept was based on a “student teacher concept”. The safety pilot can stop the experiment at any time and switch back to the mechanical flight control system by using a disengage switch at his control column or simply by moving the controls against the resistance of a force sensor. The aircrafts basic parameters are:
max PAX/min crew: 44/2
range: 1800 km
wing span: 21.5 m
length: 20.6 m
height: 7.84 m
wing area: 64 m2
MTOM: 20 800 kg
VMO: 288 KCAS (MMO: 0.63)
max. altitude: 25 000 ft (7600 m)

The test aircraft provided sufficient payload capacity and cabin space even for heavy and voluminous experimental equipment. Experimental software could easily be developed using MATLAB® / Simulink® environment. Via the MATLAB Real-Time Workshop® real-time code could be generated and transferred into the ATTAS data processing environment in a short time. In general the experimental software then was verified in the ATTAS system simulator on ground which was also used to check out and train the complete run of the experiment and to fix the final flight test carts.

Altogether 193 flight test campaigns were performed on ATTAS which gives roughly 7.5 campaigns per year with numerous sorties. In more than half of the projects the Institute of Flight Systems was involved. There is a broad range of experiments, e.g. flights with g-loads control, PIO investigations, remotely guided UAV in civil airspace and many more. From those experiments a very limited selection will be presented to underline the versatile capabilities of this marvelous aircraft.



Copyright © 2024 | Question? webmaster@acgsc.org