High performance bounded control synthesis with application to the F18 HARV

Piero Miotto; J. Marc Shewchun; Eric Feron; James D. Paduano

doi:10.2514/6.1996-3693

High performance bounded control synthesis with application to the F18 HARV

Piero Miotto, J. Marc Shewchun, Eric Feron, James D. Paduano

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

6 Scopus citations

Abstract

Designing high-performance controllers that do not saturate remains a challenge that cannot be addressed by linear control theory alone. This paper presents a control design methodology by which increasingly aggressive gains are used as the system converges to equilibrium. Stability of the resulting nonlinear control law is proved via the construction of a corresponding Lyapunov function. Performance and practicality is demonstrated by using the method to design a lateral-directional controller for the F18 HARV, using simulations models provided by NASA Dryden Flight Research Center.

Original language	English (US)
Title of host publication	1996 Guidance, Navigation, and Control Conference and Exhibit
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
Pages	1-8
Number of pages	8
DOIs	https://doi.org/10.2514/6.1996-3693
State	Published - Jan 1 1996
Externally published	Yes

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10.2514/6.1996-3693

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title = "High performance bounded control synthesis with application to the F18 HARV",

abstract = "Designing high-performance controllers that do not saturate remains a challenge that cannot be addressed by linear control theory alone. This paper presents a control design methodology by which increasingly aggressive gains are used as the system converges to equilibrium. Stability of the resulting nonlinear control law is proved via the construction of a corresponding Lyapunov function. Performance and practicality is demonstrated by using the method to design a lateral-directional controller for the F18 HARV, using simulations models provided by NASA Dryden Flight Research Center.",

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AU - Paduano, James D.

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N2 - Designing high-performance controllers that do not saturate remains a challenge that cannot be addressed by linear control theory alone. This paper presents a control design methodology by which increasingly aggressive gains are used as the system converges to equilibrium. Stability of the resulting nonlinear control law is proved via the construction of a corresponding Lyapunov function. Performance and practicality is demonstrated by using the method to design a lateral-directional controller for the F18 HARV, using simulations models provided by NASA Dryden Flight Research Center.

AB - Designing high-performance controllers that do not saturate remains a challenge that cannot be addressed by linear control theory alone. This paper presents a control design methodology by which increasingly aggressive gains are used as the system converges to equilibrium. Stability of the resulting nonlinear control law is proved via the construction of a corresponding Lyapunov function. Performance and practicality is demonstrated by using the method to design a lateral-directional controller for the F18 HARV, using simulations models provided by NASA Dryden Flight Research Center.

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BT - 1996 Guidance, Navigation, and Control Conference and Exhibit

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

ER -

High performance bounded control synthesis with application to the F18 HARV

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