1. Functional Decomposition: Part 1
The Aircraft: Fly a required flight path while carrying a payload.
Land within required distance
Take-off within required distance
Obtain required lift
Trim aircraft (longitudinal, directional, lateral)
Obtain required lift
Decrease Velocity
Obtain required initial velocity
Utilize control
surfaces
Utilize control surfaces
Utilize control surfaces
Eliminate engine thrust
Rotate ailerons as required
Thrust engine (max)
Deploy flaps
Rotate elevator (-)
Pitch aircraft up (drag increase)
Rotate elevator as required
Deploy flaps
Utilize 6 cell (22.2 volt) Lithium Polymer (Li-Poly/Li-Po) battery
Rotate rudder as required
Rotate elevator (-)

2. Functional Decomposition: Part 2
The Aircraft: Fly a required flight path while carrying a payload.
Maneuver in flight
Carry payload
Obtain required lift
Utilize payload bay
Trim aircraft
Control Aircraft
Utilize control surfaces
Maintain cruise velocity
Pitch aircraft
Roll Aircraft
Turn directionally
Attach to aircraft in a manner that it is easily loaded and removed
Thrust engine as required
Rotate elevator as required
Utilize 6 cell (22.2 volt) Lithium Polymer (Li-Poly/Li-Po) battery
Deflect ailerons as required
Rotate rudder as required
Deflect ailerons as required
Rotate rudder as required
Rotate elevator as required

3. Morphological Chart

4. Possible Solutions Schematics

5. University of Manitoba 2014 Aircraft
Pugh Selection Chart
Datum:
University of Manitoba 2014 Aircraft

6. Preliminary Flight Conditions

7. Preliminary Wing Design: Iteration 1

8. Feasibility: Take-Off and Landing Distance