Dynamically Scaled Flight and Wind Tunnel Model of a Modular UAV for Scientific Flight Experiments

Design, construct, and test dynamically scaled aircraft - both a wind tunnel model and a flight model - of an existing Dynamically scaled UAV for scientific flight experiments:
Modular design
Variable wing sweep angle
Variable tail volume
Movable landing gear
Movable engine mounts
Low weight
Secondary goals:
Outfit the plane with a variety of sensor/instrumentation systems
Implement autopilot system