1 / 22

Computer Based Aircraft Stability Control System with Manual User Navigation

Belmonte, Mark Edward C. Factora , Michael P. Neuda , Kelly Roland V. Tiam Watt, Christopher S. Villanueva, Jezrel Paul L. Mr. Clement Y. Ong ADVISER. Computer Based Aircraft Stability Control System with Manual User Navigation.

thane-nielsen
Download Presentation

Computer Based Aircraft Stability Control System with Manual User Navigation

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Belmonte, Mark Edward C. Factora, Michael P. Neuda, Kelly Roland V. Tiam Watt, Christopher S. Villanueva, Jezrel Paul L. Mr. Clement Y. Ong ADVISER Computer Based Aircraft Stability Control System with Manual User Navigation

  2. Computer Based Aircraft Stability Control System with Manual User Navigation

  3. Computer Based Aircraft Stability Control System with Manual User Navigation

  4. Six-channel radio-controlled helicopters provide versatility and maneuverability compared to other aerial crafts; however, these RC crafts are very difficult to control especially for a beginner pilot The control system to be constructed aims to provide ease of control to the pilot without removing any of the advanced features of the aircraft. Computer Based Aircraft Stability Control System with Manual User Navigation

  5. SYSTEM IMPLEMENTATION

  6. PiloT Joystick

  7. RF Transceiver

  8. RF Transceiver RF controller measured resistance

  9. Inertial measurement unit Atomic 6 DOF IMU XBee Ready

  10. Mounted on the helicopter to measure translational and rotational movement Powered by a 3.4 – 10 VDC Li-Po Cell Has a triple axis accelerometer and 3 single-axis gyroscope Atomic 6 DOF IMU XBee Ready

  11. XBee Transceiver

  12. XBEE is a wireless serial technology A wireless communications standard, which has longer range than bluetooth but lower power consumption than WiFi One is mounted on the IMU to transmit flight data while the other one is included in the ground station to receive flight data XBee Transceiver

  13. Constants: Thrust at Hover versus Inflow Velocity

  14. Thrust at Hover versus Inflow Velocity

  15. Thrust at Hover versus Inflow Velocity

  16. Thrust at Hover versus Inflow Velocity

  17. Thrust at Hover versus Inflow Velocity

  18. Thrust at Hover versus Inflow Velocity

  19. Thrust at Hover versus Inflow Velocity

  20. Thrust at Hover versus Inflow Velocity

  21. THANK YOU

  22. Belmonte, Mark Edward C. Factora, Michael P. Neuda, Kelly Roland V. Tiam Watt, Christopher S. Villanueva, Jezrel Paul L. Mr. Clement Y. Ong ADVISER Computer Based Aircraft Stability Control System with Manual User Navigation

More Related