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Design Model Validation for Small UAS VTOL using Flight Test Data
Andrew Loughran
, Thomas L. Jones
,
Simon W. Miller
,
Julia A. Cole
Research output
:
Chapter in Book/Report/Conference proceeding
›
Conference contribution
5
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Scopus citations
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Dive into the research topics of 'Design Model Validation for Small UAS VTOL using Flight Test Data'. Together they form a unique fingerprint.
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Keyphrases
Civil Applications
25%
Cost Model
25%
Design Model
100%
Efficiency Prediction
25%
Fixed-wing
50%
Flight Test Data
100%
Flight Testing
25%
Forward Flight
75%
Fuselage
25%
Hovering
25%
Hovering Flight
50%
Landing Vehicle
25%
Low Computational Cost
25%
Lower Order
25%
Means Testing
50%
Military Applications
25%
Model Prediction
50%
Model Validation
100%
Momentum Theory
25%
Performance Weight
25%
Power Draw
75%
Prediction Accuracy
25%
Prediction Power
25%
Propeller Efficiency
25%
Propeller Model
25%
Propulsive Performance
25%
Small UAS
100%
Small Unmanned Aircraft Systems (sUAS)
75%
Total Weight
25%
Vehicle Components
25%
Vertical Landing
100%
Vertical Takeoff
100%
Weight Comparison
25%
Weighted Model
25%
Engineering
Accurate Prediction
25%
Computational Cost
25%
Design Model
100%
Fixed Wings
50%
Flight Test
100%
Forward Flight
75%
Model Prediction
50%
Momentum Theory
25%
Power Draw
75%
Small Unmanned Aircraft
75%
Speed Controller
50%
Test Data
100%
Test Result
25%
Unmanned Aircraft System
100%