QFT force loop design for the aerodynamic load simulator

IEEE Transactions on Aerospace and Electronic Systems

Volumn 37, Issue 4, 2001, Pages 1384-1392

  Nam, Yoonsu ^a  

^a Kangwon National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; COMPUTER SIMULATION; FEEDBACK CONTROL; FLIGHT DYNAMICS; FORCE CONTROL; HYDRAULIC CONTROL EQUIPMENT; MATHEMATICAL MODELS; METHOD OF MOMENTS; ROBUSTNESS (CONTROL SYSTEMS);

DYNAMIC LOAD SIMULATORS (DLS); QUANTITATIVE FEEDBACK THEORY (QFT);

CONTROL SYSTEM ANALYSIS;

EID: 0035493377     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.976973     Document Type: Article

References (11)

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