Their first U . S . patent, 821, 393, did not claim invention of a flying machine, but rather, the invention of a system of aerodynamic control that manipulated a flying machine's surfaces.
32.
To perform turns, aircraft that use no thrust vectoring must rely on aerodynamic control surfaces only, such as ailerons or elevator; craft with vectoring must still use control surfaces, but to a lesser extent.
33.
The use of electric power can permit sophisticated control effects such as retracting undercarriage, operating flaps, etc . However the limited degree of freedom of the tethered model precludes the use of full aerodynamic control.
34.
A Spaceplane is a craft that is able to fly in the atmosphere like an aeroplane and is also able to reach space and manoeuvre as a spacecraft where conventional aerodynamic controls lose their effectiveness.
35.
-- > wing warping, in 1906 the United States granted an expansive patent to the Wright Brothers of Dayton, Ohio for the invention of a system of aerodynamic control that manipulated an airplane's control surfaces.
36.
The altitude was too high ( and thus the atmosphere too thin ) for the roll to cause significant aerodynamic stress, and it was correspondingly infeasible to damp the roll rate using the aerodynamic control surfaces.
37.
There are four small aerodynamic control surfaces, also in a cruciform pattern, mounted on the motor, which are connected to the guidance unit at the front of the missile via control lines running along the body.
38.
When in forward flight, the Aeroscraft is controlled by the aerodynamic control surfaces ( vertical stabilizers, empennages and canards ); however, the low speed control system aids the pilot in lower wind conditions such as during VTOL and hover.
39.
The issue of control was correctly seen as critical by the Wrights, and they acquired a wide American patent intended to give them ownership of basic aerodynamic control, despite the brothers'( and others in the aforementioned British technology patent from 1868.
40.
Reports suggest that the Had�s trajectory is kept low, so that the aerodynamic control fins at the rear of the missile can alter the trajectory and range during flight as well as making evasive maneuvres during the terminal phase near the target.
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