
aircraft control



thrust/force vector at 10 points: (due to forward movement)
	top center of each wing
	4 points around the front
	4 points around the back
	
thrust/force vector due to
	control surfaces (available range)
	wing lift (current speed, orientation)
	engines (available range)

moments of inertia around each axis


stall orientations
stall receovery

landing/takeoff envelopes, ground dist travel etc.
	
