Abstract

Abstract. Small UAV autonomous flight control system is the core part of it, so the design of the control law under the flight control system is especially important.UAV control law design can be divided into longitudinal control law design and horizontal lateral control law design.This design is mainly aimed at the longitudinal control system, study the structure and control scheme.Design the longitudinal pitch attitude control law and highly keep modal control law. Finally in Angle of pitching control, for example, designed the PID parameters based on genetic algorithm to choose optimal control, by comparing the simulation, verify the feasibility of the algorithm.

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