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A skid‐to‐turn missile autopilot design: The generalized predictive adaptive control approach
Author(s) -
Bendotti P.,
M'Saad M.
Publication year - 1993
Publication title -
international journal of adaptive control and signal processing
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.73
H-Index - 66
eISSN - 1099-1115
pISSN - 0890-6327
DOI - 10.1002/acs.4480070103
Subject(s) - skid (aerodynamics) , control theory (sociology) , autopilot , model predictive control , missile , engineering , adaptive control , control engineering , computer science , control (management) , artificial intelligence , aerospace engineering , mechanical engineering
This paper deals with an adaptive control application involving a skid‐to‐turn (STT) missile. More specifically, the generalized predictive adaptive control approach is used to accommodate the yaw channel control problem. The time domain behaviour and stability margins are shown to demonstrate the adaptive control performances vis‐a‐vis those of the underlying fixed parameter control.