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Optimization of MiG27 drone for long-range high-load flight week 9 Valentine Okonkwo Mohammad Shahid Jean-Paul Davet Tai Quach.

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Presentation on theme: "Optimization of MiG27 drone for long-range high-load flight week 9 Valentine Okonkwo Mohammad Shahid Jean-Paul Davet Tai Quach."— Presentation transcript:

1 Optimization of MiG27 drone for long-range high-load flight week 9 Valentine Okonkwo Mohammad Shahid Jean-Paul Davet Tai Quach

2 Individual and team assignments from the previous week meeting MAX 712/713 (Jean-Paul and Tai) Solar cells and Styrofoam (Valentine and Mohammad) Finish the tail section with the elevator and servo lever (Jean-Paul and Valentine) Take actual measurement of the current draw with the specific weight force of the servo (Jean-Paul, Valentine, Mohammad and Tai). Complete the simulation flight test for the force of the rudder, by using a car that is traveling at 65mph (Jean- Paul, Valentine, Mohammad and Tai). Team must decide what charge rate to use by the end of the week, and components must be ordered from mouser. (Jean-Paul and Tai) Start the installation of the landing gears (Jean-Paul and Valentine).

3 Obtained results and problems Jean Paul: Front gear support wall for control servo, Front gear assembled, main gear mount support, main gears assembled ( with valentine ), Control arms and cables routed for servo control and reinforced for support, Servo mounts built and reinforced for three servos ( with Tai), Back tail glued, Rudder glued, Servo #1 mounted and connected with cable for rudder and Controllable front wheel, Servo # 2 mounted and connected with cable for Elevator, Servo # 3 mounted and connected to cable for Throttle, Both Ailerons for wing covered with aerokote measured experimental values for maximum current to be 250ma for the overall servo control system requirements at 65 mph & Max 712 Mohammad: Solar cells and Styrofoam, Support wall is complete for front controllable wheel, Servo locations are considered and planned

4 Obtained results and problems Tai: Control arms and cables routed for servo control and reinforced for support, Servo mounts built and reinforced for three servos (with Jean Paul) Valentine: Front gear support wall for control servo, Front gear assembled, main gear mount support, main gears assembled ( with Jean- Paul), Solar cells and Styrofoam.

5 Team’s assessment of previous week task completion. Complete : 1) Front gear support wall for control servo. 2) Front gear assembled. 3) main gear mount support 4) main gears assembled 5) Control arms and cables routed for servo control and reinforced for suppport 6) Servo mounts built and reinforced for three servos 7) Back tail glued 8) Rudder glued 9) Servo #1 mounted and connected with cable for rudder and Controllable front wheel 10) Servo # 2 mounted and connected with cable for Elevator 11) Servo # 3 mounted and connected to cable for Throttle 12) Both Ailerons for wing covered with aerokote

6 Table Overall Tasks Week 123456789101112131415 Discussion /Meeting XX Turn in the paper about project X Order parts XX Sanding paper X Work on the tail on rudder section XXXX Install motor with blind nut X Sufficiency of solar cells. XXX Max 712 XXX Installation of the landing gears X Order parts for charger XX Testing Subsystem XXXX System Testing/Adjustment XX Test Flight/Adjustment XX Demonstrate of drone X

7 Team tasks for the next week 1) Ailerons need to be assembled with hinges to the main wing 2) Implantation of the servo within the wing with wood supports 3) Servo Arms and push rods assembled 4) Aerokote covering of the fuselage

8 Time accounting NameTasksTotal Hours Jean-PaulThe task 1-12 (From slide 5) Max 712 13 TaiPower point Slides Finish the tail section with the elevator and servo lever Task 5-6 (Slide 5) 7 Valentine The minutes of the meeting Solar cells and Styrofoam Front gear support wall for control servo Front gear assembled Main gear mount support & main gears assembled 11.5 MohammadSend log book by email Solar cells and Styrofoam Servo locations are considered and planned 8 Total Hour 39.5


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