Force control system design for aerodynamic load simulator

Control Engineering Practice

Volumn 10, Issue 5, 2002, Pages 549-558

  Nam, Yoonsu ^a   Hong, Sung Kyung ^b  

^a Kangwon National University   (South Korea)

^b Sejong University   (South Korea)

Author keywords

Aerodynamic load simulator; Force control; Hinge moment; Hydraulic actuator; QFT

Indexed keywords

AERODYNAMIC LOADS; COMPUTER SIMULATION; FEEDBACK CONTROL; FLIGHT SIMULATORS; MANEUVERABILITY;

FORCE CONTROLLERS; QUANTITATIVE FEEDBACK THEORY (QFT);

FORCE CONTROL;

AERODYNAMICS; AIRCRAFT; LOAD;

EID: 0036564524     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(02)00004-7     Document Type: Article

References (10)

1. Development of the direct drive valve (DDV) actuation system on the IDF aircraft
2. Full envelope flight control system design using quantitative feedback theory
3. Flight control actuation system for B-2 advanced technology bomber
4. Quantitative feedback theory with a scheduled gain for full envelope longitudinal control
5. Redundancy management concepts for advanced actuation systems