Skip to main content

Table 5 Control gain for each operation

From: Flight simulation from takeoff to yawing of eVTOL airplane with coaxial propellers by fluid-rigid body interaction

 

Control target

\(K_{p}\)

\(K_{d}\)

Throttle

v

\(2\times 10^{4}\)

\(1\times 10^{4}\)

Aileron

p

\(3\times 10^{2}\)

\(1\times 10^{2}\)

Rudder

q

\(5\times 10^{3}\)

\(8\times 10^{3}\)

Elevator

r

\(2\times 10^{3}\)

\(8\times 10^{2}\)