vtol presentation
TRANSCRIPT
Designing a Grapgical User Interface in LabVIEW to control a Vertical Take Off and Landing system
(VTOL)
Analyzation0 -27
0.1 -27
0.2 -27
0.3 -27
0.4 -27
0.5 -27
0.6 -24.6
0.7 -21
0.8 -19.1
0.9 -17.94
1 -16
1.1 -11
1.2 -6.6
1.3 -5
1.4 -3.7
1.5 -2.3
1.6 0
1.7 6.5
1.8 9
1.9 10.5
2 12
2.1 13.5
2.2 15.7
2.3 17.5
2.4 19
2.5 20.6
Voltage Angle
Counterweight is placed at 6.3 cm from the encoder shaft