Sina-1
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I guess I have to take your word for it!
Not really.
In aviation, controls are in 3 axes -- x y z -- and there is no way to get around that.
In most aircraft designs, we have discrete flight controls structures for each axis. If we eliminate one axis of controls, the aircraft would depart from controlled flight. There is no way to get around that.
So for most designs, we have the main wings to provide lift and on the wings, we have discrete flight control structures to alter the wings' shapes. These structures are leading edge (LE) and trailing edge (TE) flaps, and ailerons. Each of these structures have its own mechanical actuator.
Next are the horizontal stabilizers. They provide most of the maneuverability and they come in pairs. Two mechanical actuators.
Next is/are the vertical stabilizer(s). Each have its own mechanical actuator.
For the flying wing using split ailerons method to maintain yaw axis stability and control, we physically relocate the vertical stabilizers' mechanical actuators to be logically parallel with the wing ailerons' mechanical actuators. Then via software, we move the ailerons when needed.
The concept is not new. With the F-18 Super Hornet, we eliminated the actual speedbrake structure and uses all flight control surfaces in precise coordination with each other so that all of them act as speebrake.
https://www.ausairpower.net/SuperBug.html
With the F-18 SH, we literally eliminated the speedbrake structure and its hydraulic actuator. Two major physical components removed.
For the B-2 flying wing design, we did not eliminate the yaw axis but with software, we logically relocated the yaw axis vertical stabilizer to inside the ailerons'. It is a corollary to the F-18SH's flight controls system that eliminated the speedbrake phyiscal structure.
Again, Thanks for going through the fundamentals, however you did not provide a rebuttal to the point that I made. If flying wing (without vt) is not more expensive/complex to produce/operate then how come the vast majority of UCAVs and uavs are of a more conventional design?
The flying wing design have long range attribute before radar was invented. The RQ-170 was intended to exploit that attribute. Yes, the longer the RQ remains undetected, the longer it will be able to provide intelligence. But what good is an airborne intelligence asset if it cannot remain flying for distance and time?
Still doesn’t explain why other UCAVs/uavs operated where long range is the most desired attribute do not adopt a flying wing configuration. Let me give you a hint: it’s not worth it if stealth also is not a desired attribute