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 101 - Salt Lake City - March 2008
Agenda Location4 GENERAL COMMITTEE TECHNICAL SESSION
4.2 Research Institutions, Industry, and University Reports
4.2.2 Universities
4.2.2.2 Georgia Tech
TitleGeorgia Tech
PresenterMarc Costello
Available Downloads*presentation
*Downloads are available to members who are logged in and either Active or attended this meeting.
AbstractAn overview description of two new control mechanisms for air vehicles is provided, namely, glide slope control for parafoils and internal moving mass control for smart weapons. For autonomous parafoil and payload aircraft, control is typically created by deflection of right and left side brakes. This control mechanism achieves only lateral control. By adding an extra actuator, dynamic incidence angle control of the canopy can be achieved thus enabling active glide slope control. This capability can improve air drop accuracy by a factor of 3. For small smart weapons, the active control mechanism must be small and rugged while still achieving required control authority. By translating an internal mass, it is possible to induced predictable angular motion which in turn generates significant projectile swerve. This swerve is competitive with other smart weapon control mechanisms.



Copyright © 2024 | Question? webmaster@acgsc.org