Gain-scheduled control of a skid-to-turn missile: relaxing slow variation requirements by velocity-based design

D.J. Leith; W.E. Leithead

doi:10.1109/ACC.2001.945594

Gain-scheduled control of a skid-to-turn missile: relaxing slow variation requirements by velocity-based design

D.J. Leith, W.E. Leithead

Electronic And Electrical Engineering

Research output: Contribution to conference › Paper › peer-review

3 Citations (Scopus)

Abstract

Investigates the extension of the gain-scheduling approach to flight control tasks where the conditions required by conventional techniques need not be satisfied. In particular, situations are considered where the vehicle, is manoeuvring aggressively far from equilibrium, the airspeed need not be slowly varying and/or scheduling on the instantaneous incidence angle is required

Original language	English
Pages	500-505
Number of pages	6
DOIs	https://doi.org/10.1109/ACC.2001.945594
Publication status	Published - 25 Jun 2001
Event	American Control Conference - Arlington, VA Duration: 25 Jun 2001 → 27 Jun 2001

Conference

Conference	American Control Conference
City	Arlington, VA
Period	25/06/01 → 27/06/01

Keywords

missile engineering
skid to turn missile
flight control
velocity control
aerodynamics

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10.1109/ACC.2001.945594

Cite this

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title = "Gain-scheduled control of a skid-to-turn missile: relaxing slow variation requirements by velocity-based design",

abstract = "Investigates the extension of the gain-scheduling approach to flight control tasks where the conditions required by conventional techniques need not be satisfied. In particular, situations are considered where the vehicle, is manoeuvring aggressively far from equilibrium, the airspeed need not be slowly varying and/or scheduling on the instantaneous incidence angle is required",

keywords = "missile engineering, skid to turn missile, flight control, velocity control , aerodynamics ",

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N2 - Investigates the extension of the gain-scheduling approach to flight control tasks where the conditions required by conventional techniques need not be satisfied. In particular, situations are considered where the vehicle, is manoeuvring aggressively far from equilibrium, the airspeed need not be slowly varying and/or scheduling on the instantaneous incidence angle is required

AB - Investigates the extension of the gain-scheduling approach to flight control tasks where the conditions required by conventional techniques need not be satisfied. In particular, situations are considered where the vehicle, is manoeuvring aggressively far from equilibrium, the airspeed need not be slowly varying and/or scheduling on the instantaneous incidence angle is required

KW - missile engineering

KW - skid to turn missile

KW - flight control

KW - velocity control

KW - aerodynamics

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Gain-scheduled control of a skid-to-turn missile: relaxing slow variation requirements by velocity-based design

Abstract

Conference

Keywords

Access to Document

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Cite this