A nonlinear flight controller design for a UFO by trajectory linearization method part II-controller design

Proceedings of the Annual Southeastern Symposium on System Theory

Volumn 2002-January, Issue , 2002, Pages 103-107

  Wu, Xiaofei ^a   Adami, Tony ^a   Campbell, Jacob ^a   Jianwei, Guan ^a   Zhu, J J ^a  

^a OHIO UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE CONTROL; CONTROL THEORY; ERRORS; FEEDBACK CONTROL; FLIGHT PATHS; INVERSE PROBLEMS; LINEARIZATION; SYSTEM THEORY; TIME VARYING CONTROL SYSTEMS; TRACKING (POSITION); TRAJECTORIES;

ATTITUDE CONTROLLER; DECOUPLING CONTROLS; EIGENSTRUCTURE ASSIGNMENT; LINEAR TIME VARYING; NONLINEAR FLIGHT CONTROLLERS; TIME- VARYING BANDWIDTHS; TRACKING ERROR DYNAMICS; TRAJECTORY LINEARIZATIONS;

CONTROLLERS;

EID: 84948659906     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/SSST.2002.1027014     Document Type: Conference Paper

References (4)

1. Nelson, R., Flight Stability and Automatic Control, Second Edition, WCB/McGraw-Hill, 1998.
2. Zhu, J., Project Assignment, EE610, Aerospace Control Systems, School of EECS, Ohio University, Winter, 2001.
3. Zhu, J., Nonlinear tracking and de-coupling be trajectory linearization, Lecture Note, Presented at NASA Marshall Space Flight Center, June 1998.
4. A Nonlinear Flight Controller Design for a UFO by Trajectory Linearization method Part l-modeling.