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All figures (9)
Fig. 6. Sweep angle and switching signal.
Fig. 7. Command signal and responses.
Fig. 2. Variable sweep wing morphing aircraft.
Fig. 5. Amplified counterpart.
Fig. 4. Step response of angle of attack.
Fig. 3. Weighted interconnection of morphing aircraft.
Fig. 1. Switching regions with dwell time.
Fig. 8. Pitch rate response.
Fig. 9. Elevator deflection.
Journal Article
•
DOI
•
Switching LPV control design with MDADT and its application to a morphing aircraft
[...]
Yong He
,
Chunjuan Li
,
Weiguo Zhang
,
Jingping Shi
,
Yongxi Lü
- Show less
+1 more
06 Feb 2017
-
Kybernetika