Skip to Main Content
 

Global Search Box

 
 
 
 

ETD Abstract Container

Abstract Header

ROBUST FLIGHT CONTROL FOR COORDINATED TURNS

SARAF, ADITYA

Abstract Details

2003, MS, University of Cincinnati, Engineering : Aerospace Engineering.
In this thesis, the coupled, six-degree-of-freedom, motion equations for a fighter-type aircraft are derived and linearized for a typical subsonic cruise condition involving a coordinated turn at a steady turn rate. Because of the nonzero turn rate and the nonzero roll angle required for it, the equations of motion are coupled and therefore cannot be treated as decoupled longitudinal and lateral motions, particularly for relatively large turn rates. The linearized, coupled motion equations are then used to design a robust linear feedback controller for a particular turn rate using the LQG/LTR design technique. The robust controller is applied to the dynamics at other, considerably different turn rates, demonstrating its robustness. Although a sufficient condition for robust stability is violated over part of the frequency range, less conservative analysis of the closed loop system using structured singular value shows that the controller-plant system is robust to operating point changes.
Dr. Bruce Walker (Advisor)
70 p.

Recommended Citations

Citations

  • SARAF, A. (2003). ROBUST FLIGHT CONTROL FOR COORDINATED TURNS [Master's thesis, University of Cincinnati]. OhioLINK Electronic Theses and Dissertations Center. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1060883331

    APA Style (7th edition)

  • SARAF, ADITYA. ROBUST FLIGHT CONTROL FOR COORDINATED TURNS. 2003. University of Cincinnati, Master's thesis. OhioLINK Electronic Theses and Dissertations Center, http://rave.ohiolink.edu/etdc/view?acc_num=ucin1060883331.

    MLA Style (8th edition)

  • SARAF, ADITYA. "ROBUST FLIGHT CONTROL FOR COORDINATED TURNS." Master's thesis, University of Cincinnati, 2003. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1060883331

    Chicago Manual of Style (17th edition)