This paper presents a novel design of optimal flight control for a two-degree-of-freedom helicopter. The linear-quadratic-regulator (LQR) technology is applied to control the pitch motion of the helicopter. The particle swarm optimization (PSO) is employed to search the optimal weighting matrices of the LQR controller. Computer simulations demonstrate the flight performance will be optimal by means of the LQR control based on PSO.
Optimal Design of Helicopter Control Systems Using Particle Swarm Optimization
2019-05-01
273604 byte
Conference paper
Electronic Resource
English
CONTROL SYSTEM DESIGN FOR AN AUTONOMOUS HELICOPTER USING PARTICLE SWARM OPTIMIZATION
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