Trajectory scheduled missile autopilot design

J.S. Shamma; J.R. Cloutier; IEEE

doi:10.1109/CCA.1992.269870

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Conference proceeding

Trajectory scheduled missile autopilot design

J.S. Shamma, J.R. Cloutier and IEEE

[Proceedings 1992] The First IEEE Conference on Control Applications, pp.237-242 vol.1

1992

DOI: https://doi.org/10.1109/CCA.1992.269870

Abstract

Aerodynamics

Control design

Control systems

Costs

Dynamic scheduling

Force control

History

Linear approximation

Missiles

Stability

An alternate approach to the design of gain-scheduled controllers is given. Standard gain-scheduling typically relies on the instantaneous value of the scheduling variable to update the control gains. This approach has the drawbacks of being limited to slow transitions between operating points and requiring a number of possibly tedious point-by-point designs. The present approach is to have the controller gains dynamically evolve according to the scheduling variable's history, rather than its instantaneous value. At the cost of increased order of the controller, this approach allows rapid transitions between operating conditions and alleviates the need for several point-by-point designs. The approach is demonstrated via a stabilizing control design for a longitudinal missile model.< >

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Details

Title: Trajectory scheduled missile autopilot design
Creators - without role: J.S. Shamma - The University of Texas at Austin
J.R. Cloutier - United States Air Force Research Laboratory
IEEE
Publication Details: [Proceedings 1992] The First IEEE Conference on Control Applications, pp.237-242 vol.1
Publisher: IEEE
Identifiers: 9945149008331
Academic Unit: King Abdullah University of Science & Technology
Language: English
Resource Type: Conference proceeding