QNET Vertical Take-Off and Landing (VTOL)
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Transcript of QNET Vertical Take-Off and Landing (VTOL)
![Page 1: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/1.jpg)
QNET VTOL Trainer
Project 2
By Fadzli,John & Zoubair
|
CURRENTCONTROL
FIGHT CONTROL
MODELING
RESULTS
![Page 2: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/2.jpg)
Current Control
LAB Section Name Slide No.
1. Finding resistance 3
2.Qualitative Current Control
6
3.Current Control Design
8
4. Result 7
![Page 3: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/3.jpg)
• Current Control off
• Vary Voltage 4 to 8v
• Find the current & resistance
Ohm’s Law
Finding A & OHm
Current
R = 4 / 1.6
R = 2..5 ohm
![Page 4: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/4.jpg)
• Current Control off
• Vary Voltage 4 to 8v
• Find the current & resistance
Measurement Graphs tab
find the steady-state gain and the time
constant
Finding A & OHm
R = 5 / 1.9
R = 2.63 ohm
![Page 5: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/5.jpg)
• Current Control off
• Vary Voltage 4 to 8v
• Find the current & resistance
Measurement Graphs tab
find the steady-state gain and the time
constant
Finding A & OHm
R = 6 / 2.3
R = 2.61 ohm
![Page 6: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/6.jpg)
• Current Control off
• Vary Voltage 4 to 8v
• Find the current & resistance
Measurement Graphs tab
find the steady-state gain and the time
constant
Finding A & OHm
R = 7 / 2.8
R = 2.5 ohm
![Page 7: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/7.jpg)
• Current Control off
• Vary Voltage 4 to 8v
• Find the current & resistance
Measurement Graphs tab
find the steady-state gain and the time
constant
Finding A & OHm
R = 8 / 3.2
R = 2.5 ohm
![Page 8: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/8.jpg)
Lab 2: Qualitative Current Control
• Amplitude = 0.20 A
• Frequency = 0.40 Hz
• Offset = 0.90 A
• kp;c = 0.250
• ki;c = 10
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Lab 2: Qualitative Current Control
• kp;c = 0.250
• ki;c = 10
*• kp; c = 0
• ki; c = 100
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Calculate the PI gains, kp and ki
• Wn = 42.5 rad/s
• ç = 0.70
Lab 3: Current Control Design
Lm = 53.8 mH
Kp = 0.65
ki = 47.17
![Page 11: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/11.jpg)
• Amplitude = 0.20 A
• Frequency = 0.40 Hz
• Offset = 0.90 A
enter Ki & Kp found previously
Model validation
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Parameter Value Units
Rm 2.5 Ohm
Lm 53.8 mH
Wn 42.5 rad/s
kp;c 0.65 V/A
ki;c 97.176 V/(A s)
![Page 13: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/13.jpg)
MODELLING
LAB Section Name Slide No.
1.Measure the Equilibrium
Current 9
2. Find Natural Frequency 11
3. Model Validation 15
4. Using the System Identification Tool 16
5. Result 17
![Page 14: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/14.jpg)
Current Control ON
Pi found previously
• Amplitude = 0.00 A
• Frequency = 0.40 Hz
• Offset = 1.00 A
Gradually increase the offset current
until the VTOL Trainer is horizontal.
Lab 1: Measure the Equilibrium
Current
![Page 15: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/15.jpg)
Current Control ON
Pi found previously
• Amplitude = 0.00 A
• Frequency = 0.40 Hz
• Offset = 1.00 A
Gradually increase the offset current
until the VTOL Trainer is horizontal.
Lab 1: Measure the
Equilibrium
![Page 16: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/16.jpg)
Current Control ON
Pi found previously
• Amplitude = 0.00 A
• Frequency = 0.40 Hz
• Offset = 1.00 A
Gradually increase the offset current
until the VTOL Trainer is horizontal.
Lab 1: Measure the
Equilibrium
![Page 17: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/17.jpg)
Current Control ON
Pi found previously
• Amplitude = 0.00 A
• Frequency = 0.40 Hz
• Offset = 1.00 A
Gradually increase the offset current
until the VTOL Trainer is horizontal.
Lab 1: Measure the
Equilibrium
![Page 18: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/18.jpg)
Lab 2: Find Natural
Frequency
Current Control ON
Pi found previously
• Amplitude = 0.00 A
• Frequency = 0.40 Hz
• Offset = Ieq = 1.10
![Page 19: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/19.jpg)
Current Control ON
Pi found previously
• Amplitude = 0.00 A
• Frequency = 0.20 Hz
• Offset = Ieq = 1.10
Amplitude =0.10 A
Lab 3: Model Validation
![Page 20: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/20.jpg)
• Amplitude = 0.10 A
• Frequency = 0.20 Hz
• Offset = Ieq = 1.10
Enter the identified transfer function.
Lab 4: Using the System
Identification Tool
![Page 21: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/21.jpg)
• Amplitude = 0.10 A
• Frequency = 0.20 Hz
• Offset = Ieq = 1.10
Enter the identified transfer function.
Lab 4: Using the System
Identification Tool
![Page 22: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/22.jpg)
Description Symbol Value Unit
MODELLING
Equilibrium current Ieq 1.08 A
Torque thrust constant Kt .0209 (N m)/A
Moment of inertia J 0.0035 kg m2
Viscous damping B 0.002 (N m s)/rad
Natural frequency Wn 3.14 rad
Stiffness K 0.0345 (N m)/rad
Sys ID: Torque-thrust constant Kt 0.0196 (N m)/A
Sys ID: Viscous damping Bid 0.01 (N m s)/rad
Sys ID: Stiffness Kid 0.0343 (N m)/rad
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FIGHT CONTROL
LAB Section Name Slide No.
1. PD Steady-State Analysis 19
2.PID Steady-State Error
Analysis 11
3. PID Control Design 15
4. Result 16
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Calculate the theoretical VTOL Trainer steady-state error when
using a PD control with kp = 2 and kd = 1 and
a step amplitude of R0 = 4.0 degrees.
Lab 1: PD Steady-State
Analysis
Ess = 1.556 R0 = 4
J = 0.0035
b = 0.002
K = 0.0345
Ki = 0
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• Amplitude = 0.0 deg
• Frequency = 0.15 Hz
• Offset = 0.0 deg
• kp = 1.0 A/rad
• ki = 2 A/(rads)
• kd = 1.0 As/rad
Lab 1: PD Steady-State Analysis
![Page 26: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/26.jpg)
• kp = 2.0 A/rad
• ki = 0 A/(rad.s)
• kd = 1.0 A.s/rad
• Amplitude = 2.0 deg
• Frequency = 0.40 Hz
• Offset = 2.0 deg
Lab 1: PD Steady-State
Analysis
![Page 27: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/27.jpg)
increment the integral gain until you reach ki = 4.0 A/(rads).
Lab 1: PD Steady-State
Analysis
![Page 28: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/28.jpg)
increment the integral gain until you reach ki = 4.0 A/(rads).
Lab 2: PID Steady-State
Error
Analysis
![Page 29: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/29.jpg)
increment the integral gain until you reach ki = 4.0 A/(rads).
Lab 2: PID Steady-State Error
Analysis
![Page 30: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/30.jpg)
increment the integral gain until you reach ki = 4.0 A/(rads).
Lab 2: PID Steady-State Error
Analysis
![Page 31: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/31.jpg)
increment the integral gain until you reach ki = 4.0 A/(rads).
Lab 2: PID Steady-State Error
Analysis
![Page 32: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/32.jpg)
• Amplitude = 0.0 deg
• Frequency = 0.15 Hz
• Offset = 0.0 deg
enter the PID gains found in Section
4.5.1.
Lab 3: PID Control Design
![Page 33: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/33.jpg)
• Amplitude = 2.0 deg
• Frequency = 0.40 Hz
• Offset = 2.0 deg
Lab 3: PID Control Design
![Page 34: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/34.jpg)
set Amplitude (rad) to 0 rad and slowly decrement Offset
(rad) to -8.0 rad.
Lab 3: PID Control Design
![Page 35: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/35.jpg)
set Amplitude (rad) to 0 rad and slowly decrement Offset
(rad) to -8.0 rad.
Lab 3: PID Control Design
![Page 36: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/36.jpg)
set Amplitude (rad) to 0 rad and slowly decrement Offset
(rad) to -8.0 rad.
Lab 3: PID Control Design
![Page 37: QNET Vertical Take-Off and Landing (VTOL)](https://reader035.fdocuments.net/reader035/viewer/2022081720/55a3d8701a28abc4448b477b/html5/thumbnails/37.jpg)
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SUMMARY
Concepts learned in the Vtol Trainer
✓ Current control
✓ Modelling & Validation
✓ PID
✓ Steady state analysis