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Honeywell
Guidance, Navigation and Control Center of Excellence (COE)
SAE G&C Committee MeetingMarch 2, 2005
2 HONEYWELL - CONFIDENTIAL SP-SAE-G&C-March 2005
Spring Update
• Autonomy- Micro Air Vehicle (MAV)
First tethered flights Dec 21, 2004- Organic Air Vehicle – 2 program
commencedFocus on collision avoidance algorithms
- HURT program kicked-off
• Advanced Control- NASA CUPR program
Piloted simulations at Langley- Boeing 7e7 program
Fly-by-wire implementation- Boeing CMUS program
Technical progress reviewed
• Coordinated control- C-17 FFS program update
-11
08-12
0303
LAIL
RAIL
LELEV
RELEV
RUD
ROLL
PITCH
YAW
R AIL STUCK 8 DEGROLL LMTS SETDGD A/C PRF – POT ICINGSIG INJ – TEST R ELEV
Control Authority Display Control Surface Status Display
Integrated Message Area
ControlSurfaceDisplacementScale
NewLimits Current
Setting
NEW CSC
3 HONEYWELL - CONFIDENTIAL SP-SAE-G&C-March 2005
Intelligent Autonomy
• Micro-Air Vehicle (MAV)- Tethered flights at Honeywell’s
Albuquerque site- Challenging flight controls and
navigation problems- SMARTLabs for prototyping,
visualization
• Organic Air Vehicle (OAV-2)- Phase 1 effort ongoing- Focus on collision avoidance- Explore sensor modalities and
novel algorithms- React to pop-up obstacles
4 HONEYWELL - CONFIDENTIAL SP-SAE-G&C-March 2005
Intelligent Autonomy (contd.) – HURT program
Urban RSTA requires horizontal viewpoints and rapid reaction to cues and perceived threats
The HURT control layer can make existing vehicles behave like a distributed robotic sensor
Rapid “fly-by shooting”of concealed targets
Persistent mobile sensors
Overhead surveillance
Agile urban navigation to see in portals
Ground and subterranean recce
Cueing sensors
FUTURE UAV
Side-looking RSTA
Multilateral geolocation
LOS comms relay chain
*Courtesy of DARPA and Northrop Grumman
HURT Provides On-Demand Collaborative RSTA for Obscured Targets
5 HONEYWELL - CONFIDENTIAL SP-SAE-G&C-March 2005
Advanced Controls
• 7E7 Fly-by-wire program- Design reviews ongoing- End-to-end system modeling, redundancy
analysis
• Boeing/AFRL CMUS program- Adaptive inner loop algorithms responsive
to IVHM signals
• Second Piloted simulation at NASA Langley- Successful demonstration of CUPRSys for
3 operating points - Demonstrated benefits of reconfigurable
control Elevator faults simulated on Boeing 757 modelNominal, faulty and reconfigured cases evaluatedResults will be presented at SAE-G&C Meeting 96
6 HONEYWELL - CONFIDENTIAL SP-SAE-G&C-March 2005
Honeywell Labs CUPRSys
-11
08-12
0303
L AIL
R AIL
L ELEV
R ELEV
RUD
ROLL
PITCH
YAW
R AIL DAMAGED ROLL LMTS SET DGD A/C PRF – POT ICING SIG INJ – TEST R ELEV
Control Authority Display Control Surface Status Display
Integrated Message Area
Control Surface Displacement Scale
New Limits Current
Setting
NEW CSC
7 HONEYWELL - CONFIDENTIAL SP-SAE-G&C-March 2005
Multi-Vehicle Control
• Formation Flying System (FFS) for C-17- Ensure spacing and coordination- System level analysis and
algorithm design of TCAS-ADSB hybrid surveillance for C17 formations
- Delivered MILACAS-FR FFS Processor consignment EDU to Boeing for support test and integration
Element Lead 1(Formation Lead)
Left Wing 1
Right Wing 1
Element Lead N
Right Wing N
Left Wing N
Element Lead 2 … N-1
Right Wing 2 ... N-1
Left Wing 2 … N-1
8 HONEYWELL - CONFIDENTIAL SP-SAE-G&C-March 2005
Thank you