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 106 - La Jolla - October 2010
Agenda Location8 SUBCOMMITTEE A – AERONAUTIC AND SURFACE VEHICLES
8.2 Smart Adaptive Flight Effective Cue (SAFE-Cue)
TitleSmart Adaptive Flight Effective Cue (SAFE-Cue)
PresenterDave Klyde
AffiliationSystems Technology, Inc.
Available Downloads*presentation
*Downloads are available to members who are logged in and either Active or attended this meeting.
AbstractDavid Klyde
dklyde@systemstech.com

The Smart Adaptive Flight Effective Cue or SAFE-Cue has been developed in this program to address the challenge of adverse pilot interactions with an adaptive control system. This innovative cueing system provides force feedback to the pilot via an active control inceptor with corresponding command path gain adjustments to alert the pilot that the adaptive control system is active and provide guidance via force feedback cues to ensure pilot-vehicle system stability and performance in the presence of damage or failures. While the focus herein is on an adaptive controller, the SAFE-Cue concept is completely general and can therefore be applied to any flight control system implementation as a means to mitigate loss of control. The full scale NASA Generic Transport Model was combined with the Receding Horizon Optimal/Modified Sequential Least Squares (RHO/MSLS) adaptive control algorithm to provide the means to develop and demonstrate the SAFE-Cue system in Phase 1. The SAFE-Cue activates when the measured System Error between a model-based nominal system response and the actual adaptive control system response exceeds a defined threshold. A piloted simulation was conducted with two test pilots with significant transport aircraft experience. The results of the simulation found that pitch rate System Error measure was an effective means of distinguishing performance of the adaptive system with failure/damage and a nominal (healthy) system. Furthermore, the SAFE-Cue system was very effective at suppressing pilot-vehicle system oscillations for the given failure/damage scenarios, allowing the pilots to focus on the task at hand rather than simply maintaining control.



Copyright © 2024 | Question? webmaster@acgsc.org