A
STUDYING CONTROL SYSTEM FOR A SMALL vertical
takeoff and landing AIRCRAFT
A.S. Kulik,
S.N. Firsov, Van Thinh
Nguyen
This paper presents
a new class of small vertical takeoff and landing (VTOL) aircraft, also the control
algorithms were proposed, which provide a given quality of performance of the studied
flying vehicle in nominal condition as well as in presence of abnormal situations.
Although it presents a series of models, which reflect the peculiarities of the
small vertical takeoff and landing aircraft in the nominal condition and during
abnormal situations, that are related to the faults on the aerodynamic control
surfaces.
Keywords: small-sized
aircraft, the coordinate system, transformation matrix, microcontroller, accelerometer,
angular velocity sensor.