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Presented By:
Fahad Ali Amjad 12063122-027
Abdullah Mir 12063122-039
 This paper includes two avionic control systems.
 Implemented as educational tools in the study path of
Information Technology for Aerospace.
 They are used in ongoing development and research projects.
 These exercise systems are SCS & QCS.
 SCS means SEESAW CONTROL SYSTEM
 QCS means QUADROTOR CONTROL SYSTEM
 SCS task is to stabilize the system at desired tilt angle
and angular rate.
 To improve the system response by tuning the
controller parameters.
 Sensors are used to measure the actual output of the
system and feed this information back to the
controller.
 The controller uses this information to adjust the
signal of the system accordingly.
 3-Axis accelerometer sensor (MMA7361L)
 Driver IC for dual DC motors (TB6612FNG H-Bridge)
 Data acquisition unit (NI USB-6008)
AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT
 Software of the SCS is implemented using LabVIEW
and can be used in two main controlling tasks.
 In order to stabilize the system around a desired tilt
angle, a (Proportional Integral Derivative) PID
Controller is used to control the rotational speed of a
single motor.
 In case of two motors, the PID controller will
calculate the required ratio needs to be increased and
decreased respectively for stabilizing the system
around a desired tilt angle.
 The calibration of sensor is used to improve the quality of
data.
 SCS includes how the output of the PID controller
adjusts itself to the required input for stabilizing the
system around a desired point.
 The main idea of the QCS was to design a tool to
learn embedded programming in a real time
environment using an application from Avionics.
 In QCS, the students can do implementation step by
step and test their own control algorithm to stabilize
the system and later to use it in real flying quadrotors.
 Microcontroller UC3A Atmel.
 IM (Inertial Measurement Unit) consisting of
the ITG3200 gyroscope and the ADXL345
accelerometer.
 Four brushless controllers using the I²C.
 Uses I²C to connect all peripherals on one
bus.
 Minimum number of wires and drivers to run
the system.
AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT
 Components like magnetic compass, infrared,
ultrasonic and pressure sensors can be added
using the I²C bus.
 The microcontroller provides enough I/O
lines to connect all other kind of peripheries
like Bluetooth, Wifi, Camera, GPS etc.
 Software is designed using the Atmel
Framework (Technical Library) within AVR32
Studio.
 We can implement all levels of the softwares
to create I²C (Inter-Integrated Circuit),USART
(Universal Synchronous Asynchronous
Receiver Transmitter) etc over communication
protocols.
 The control loop operates on a sample time
10ms, fast enough for a very stable control
behavior in this application.
 The microcontroller could even handle a
faster sample time.
 Mechanical design involves different versions
of implementation and parameterizing of
each controller for all axes separately.
 In the first version, all parts of the tri-axial
controller including its parameters and
algorithm can be tested separately and
altogether.
 In the second version, the quadrotor can
manipulate its orientation in all 3 rotation
axes without changing the position meaning
the 3 translational axes.
AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT
 The QCS proved to be a successful learning
tool and was able to control and fly the
quadrotor.
 Nevertheless for an optimized flight the PID
parameters had to be adapted.
 One big issue of this approach was the use of
I²C.
 Autonomous Flying Robots, Spring 2010, Kenzo Nonami
 Introduction to Feedback Control Theory, CRC Press 1999, Hitay Özbay,
ISBN: 084931867X
 LabVIEW for Everyone, Prentice Hall 2005, James Kring, and Jeffrey
Travis, ISBN:0131856723
 AT32UC3A Series Preliminary, Datasheet Online Accessed January 2012,
http://www.atmel.com/dyn/resources/prod_documents/32058S.pdf
 Igus GmBH, http://www.igus.de
AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT

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AVIONIC CONTROL SYSTEMS FOR EDUCATION & DEVELOPMENT

  • 1. Presented By: Fahad Ali Amjad 12063122-027 Abdullah Mir 12063122-039
  • 2.  This paper includes two avionic control systems.  Implemented as educational tools in the study path of Information Technology for Aerospace.  They are used in ongoing development and research projects.
  • 3.  These exercise systems are SCS & QCS.  SCS means SEESAW CONTROL SYSTEM  QCS means QUADROTOR CONTROL SYSTEM
  • 4.  SCS task is to stabilize the system at desired tilt angle and angular rate.  To improve the system response by tuning the controller parameters.  Sensors are used to measure the actual output of the system and feed this information back to the controller.  The controller uses this information to adjust the signal of the system accordingly.
  • 5.  3-Axis accelerometer sensor (MMA7361L)  Driver IC for dual DC motors (TB6612FNG H-Bridge)  Data acquisition unit (NI USB-6008)
  • 7.  Software of the SCS is implemented using LabVIEW and can be used in two main controlling tasks.  In order to stabilize the system around a desired tilt angle, a (Proportional Integral Derivative) PID Controller is used to control the rotational speed of a single motor.  In case of two motors, the PID controller will calculate the required ratio needs to be increased and decreased respectively for stabilizing the system around a desired tilt angle.
  • 8.  The calibration of sensor is used to improve the quality of data.
  • 9.  SCS includes how the output of the PID controller adjusts itself to the required input for stabilizing the system around a desired point.
  • 10.  The main idea of the QCS was to design a tool to learn embedded programming in a real time environment using an application from Avionics.  In QCS, the students can do implementation step by step and test their own control algorithm to stabilize the system and later to use it in real flying quadrotors.
  • 11.  Microcontroller UC3A Atmel.  IM (Inertial Measurement Unit) consisting of the ITG3200 gyroscope and the ADXL345 accelerometer.  Four brushless controllers using the I²C.  Uses I²C to connect all peripherals on one bus.  Minimum number of wires and drivers to run the system.
  • 13.  Components like magnetic compass, infrared, ultrasonic and pressure sensors can be added using the I²C bus.  The microcontroller provides enough I/O lines to connect all other kind of peripheries like Bluetooth, Wifi, Camera, GPS etc.
  • 14.  Software is designed using the Atmel Framework (Technical Library) within AVR32 Studio.  We can implement all levels of the softwares to create I²C (Inter-Integrated Circuit),USART (Universal Synchronous Asynchronous Receiver Transmitter) etc over communication protocols.
  • 15.  The control loop operates on a sample time 10ms, fast enough for a very stable control behavior in this application.  The microcontroller could even handle a faster sample time.
  • 16.  Mechanical design involves different versions of implementation and parameterizing of each controller for all axes separately.  In the first version, all parts of the tri-axial controller including its parameters and algorithm can be tested separately and altogether.  In the second version, the quadrotor can manipulate its orientation in all 3 rotation axes without changing the position meaning the 3 translational axes.
  • 18.  The QCS proved to be a successful learning tool and was able to control and fly the quadrotor.  Nevertheless for an optimized flight the PID parameters had to be adapted.  One big issue of this approach was the use of I²C.
  • 19.  Autonomous Flying Robots, Spring 2010, Kenzo Nonami  Introduction to Feedback Control Theory, CRC Press 1999, Hitay Özbay, ISBN: 084931867X  LabVIEW for Everyone, Prentice Hall 2005, James Kring, and Jeffrey Travis, ISBN:0131856723  AT32UC3A Series Preliminary, Datasheet Online Accessed January 2012, http://www.atmel.com/dyn/resources/prod_documents/32058S.pdf  Igus GmBH, http://www.igus.de