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 133
(Coming Soon!)

 
 

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 106 - La Jolla - October 2010
Agenda Location4 GENERAL COMMITTEE TECHNICAL SESSION
4.2 Government Agencies Summary Reports
4.2.1 NASA
4.2.1.2 Dryden
TitleDryden
PresenterJohn Bosworth
Available Downloads*presentation
video
*Downloads are available to members who are logged in and either Active or attended this meeting.
AbstractNASA Dryden continues to support controls research through flight exploration. The F-18 Full-scale Advanced Systems Testbed (FAST) launched with a first flight of the research flight control system in March of 2010. This system is coupled with an Advanced Research Test System (ARTS) IV computer that allows for testing of auto-coded control laws from an engineering design environment. The first flight of an auto-coded nonlinear dynamic inversion controller occurred in September of 2010. Dryden has also acquired a Gulfstream III aircraft to serve as a flying testbed for aerodynamics. The first two initial experiments are a laminar flow glove to test the effectiveness of discrete roughness elements an adaptive compliant trailing edge flap for smooth lift and roll control. The X-48B Blended Wing Body vehicle has completed 80 flights and has moved on to a parameter identification flight phase that has 648 planned test points. The X-48C vehicle has completed wind tunnel testing and will investigate optimized intelligent control for performance and use of engine thrust differential for yaw control. The Stratospheric Observatory For Infrared Astronomy (SOFIA) has completed open telescope door envelope finding no significant handling qualities effects. The aircraft is ready to proceed with science missions and development of an autopilot controller that will provide tight tracking performance for science observations. A future project that is expected to fly at NASA Dryden is the Multi-Utility Technology Testbed (MUTT). This AFRL and Lockheed Martin partnership will demonstrate active flutter suppression and gust load alleviation. NASA plans to develop guidelines and methodology for active dynamic structural control and provide flight-validated aircraft models for academia. Dryden successfully led the test activities for the launch abort system tests at White Sands in New Mexico. The pad abort test occurred on May 6, 2010 and was extremely successful. Dryden involvement will continue with support for the uncrewed low earth orbit test of entry, descent and landing. Following that an ascent abort flight test is planned. Dryden continues to fly what others imagine.



Copyright © 2024 | Question? webmaster@acgsc.org