Backstepping designs for jet engine stall and surge control

Krstić, Miroslav; Protz, Jonathan M.; Paduano, James D.; Kokotović, P.V.

doi:10.1109/cdc.1995.478612

Cited by 60 publications

(24 citation statements)

References 10 publications

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“…However, for optimality » need not satisfy (10), (11) and (13). Specifically, if » is a C function such that (10) is satisfied and (x) 3S(x ), then (14) and (15) imply (16) and (17).…”

Section: Remark 33mentioning

confidence: 94%

A unification between nonlinear-nonquadratic optimal control and integrator backstepping

Haddad

Fausz

Chellaboina

et al. 1998

Int. J. Robust Nonlinear Control

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“…However, for optimality » need not satisfy (10), (11) and (13). Specifically, if » is a C function such that (10) is satisfied and (x) 3S(x ), then (14) and (15) imply (16) and (17).…”

Section: Remark 33mentioning

confidence: 94%

A unification between nonlinear-nonquadratic optimal control and integrator backstepping

Haddad

Fausz

Chellaboina

et al. 1998

Int. J. Robust Nonlinear Control

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“…Now, using , where is the ideal change in fluid specific enthalpy which, for a conservative system, is equal to the work done by the compressor rotor, it follows from (7) that (8) The energy delivered to the fluid by the compressor is given by (9) where is the angular velocity of the compressor spool and (10) where , correspond to incidence and frictional losses at the inducer and diffuser, respectively. For details see [21].…”

Section: B Conservation Of Momentummentioning

confidence: 99%

Globally stabilizing switching controllers for a centrifugal compressor model with spool dynamics

Leonessa

Haddad

2000

IEEE Trans. Contr. Syst. Technol.

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In this paper we develop a globally stabilizing stability-based switching controller for a three-state lumped parameter centrifugal compressor surge model. The proposed model involves pressure and mass flow compression system dynamics as well as spool dynamics to account for the influence of speed transients on the compression surge dynamics. The proposed nonlinear switching controller architecture involves throttle and compressor torque regulation and is directly applicable to compression systems with actuator amplitude and rate saturation constraints.

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“…The backstepping method provides a systematic procedure to find state feedback and Lyapunov function simultaneously. Several works on active surge control using backstepping have been presented afterwards [13]- [16]. However, the backstepping may result in a complicated state feedback and can be difficult to be implemented [17].…”

Section: Introductionmentioning

confidence: 99%

Compressor surge control design using linear matrix inequality approach

Uddin

Gravdahl

2017

2017 5th International Conference on Instrumentation, Control, and Automation (ICA)

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Abstract-A novel design for active compressor surge control system (ASCS) using linear matrix inequality (LMI) approach is presented and including a case study on piston-actuated active compressor surge control system (PAASCS). The nonlinear system dynamics of the PAASCS is transformed into linear parameter varying (LPV) system dynamics. The system parameters are varying as a function of the compressor performance curve slope. A compressor surge stabilization problem is then formulated as a LMI problem. Solving the LMI problem results in a feedback control gain for the compressor surge stabilization and stability proof of the closed loop system in the whole compressor operating area. Simulation results show that the designed surge control system is able to stabilize compressor surge. Significant improvement of the control system performance is achieved by combining the LMI approach and linear quadratic regulator (LQR).

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Backstepping designs for jet engine stall and surge control

Cited by 60 publications

References 10 publications

A unification between nonlinear-nonquadratic optimal control and integrator backstepping

A unification between nonlinear-nonquadratic optimal control and integrator backstepping

Globally stabilizing switching controllers for a centrifugal compressor model with spool dynamics

Compressor surge control design using linear matrix inequality approach

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