Title : 
Lean backstepping design for a jet engine compressor model
         
        
            Author : 
Krstic, Miroslav ; Kokotovic, Petar
         
        
            Author_Institution : 
Dept. of Mech. Eng., Maryland Univ., College Park, MD, USA
         
        
        
        
        
        
            Abstract : 
Backstepping offers flexibilities not present in other nonlinear design procedures. One of them is the possibility to avoid cancellation of useful nonlinearities. Such cancellations, which are common in feedback linearization designs, require large control effort and cause nonrobustness. As an illustration of a design that avoids cancellations we develop controllers for the Moore-Greitzer model of a jet engine compressor system. The resulting backstepping controllers use less control effort than feedback linearizing controllers
         
        
            Keywords : 
aerospace engines; Moore-Greitzer model; backstepping control; compressor model; feedback; jet engine; linearization; Backstepping; Bifurcation; Control nonlinearities; Educational institutions; Force control; Jet engines; Linear feedback control systems; Lyapunov method; Mechanical engineering; Surges;
         
        
        
        
            Conference_Titel : 
Control Applications, 1995., Proceedings of the 4th IEEE Conference on
         
        
            Conference_Location : 
Albany, NY
         
        
            Print_ISBN : 
0-7803-2550-8
         
        
        
            DOI : 
10.1109/CCA.1995.555901