Optimization of fuzzy controller for minimum time response

• Main Authors: Nagi F., Perumal L.
• Other Authors: 56272534200
• Format: Article
• Published: Elsevier Ltd 2023
• Subjects: Attitude control; Bang-bang; Fuzzy controller; Largest of maximum; Membership function spans; Optimization; Pneumatic rotary actuator; Real-time workshop; Self tuning parameters; Thruster; xPC target; Bang bang control systems; Fuzzy logic; Membership functions; Navigation; Pneumatic actuators; Pneumatics; Satellites; Fuzzy controllers; Real time workshop; Controllers

Minimum time control is desired for non-linear spacecraft-satellite attitude systems to save on-board thruster fuel. The regulatory time depends on the initial attitude of the satellite. Bang-bang control of satellite attitude can be accomplished with fuzzy logic controller using largest of Maxima d...