Research of program simulation flight for certain type of airplane
Hao Shun · Flight Dynamics · 2000
According to the principle of inertial navigation, navigation formula is evolved, after the integrate manipulate mode of certain type of airplane is introduced, the control process and mathematical models of simulation course are presented in this paper with control law of lean angle and simplification relationship of course and lean angle. According to gathered flight datum and flight orbit, it is concluded that mathematical models of simulation course are correct to realizing automatic flight among the planned route spots known as program simulation flight and can be used as a reference in studying navigation software.