Design of blended control strategy for missiles with lateral jets and aerodynamic surfaces

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 31, Issue 4, 2010, Pages 701-708

  Yao, Yu ^a   Bi, Yongtao ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Active disturbance rejection control; Attitude control system; Dynamic inversion; Integer programming; Pulse moter

Indexed keywords

ACTIVE DISTURBANCE REJECTION CONTROLS; AERODYNAMIC CONTROL; AERODYNAMIC SURFACES; CONTROL STRATEGIES; FAST RESPONSE; HIGH PRECISION; INTEGER LINEAR PROGRAMMING; LATERAL JET; LATERAL JET INTERACTION; LATERAL THRUST; NON-LINEARITY; ON DYNAMICS; PARAMETER UNCERTAINTY; PITCH CHANNELS; RESPONSE PROCESS; SIDESLIP ANGLES; SIMULATION RESULT; SPINNING MISSILES; STRONG COUPLING;

ANGLE OF ATTACK; ATTITUDE CONTROL; COMMUNICATION SATELLITES; CONTROL SYSTEMS; DEGREES OF FREEDOM (MECHANICS); DISTURBANCE REJECTION; FLOW PATTERNS; GAS DYNAMICS; LINEARIZATION; MISSILES; NAVIGATION; RECEPTION QUALITY; SPATIAL VARIABLES CONTROL;

INTEGER PROGRAMMING;

EID: 77952666800     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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