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

D.J. Leith, W.E. Leithead

Research output: Contribution to conferencePaper

2 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 languageEnglish
Pages500-505
Number of pages6
DOIs
Publication statusPublished - 25 Jun 2001
EventAmerican Control Conference - Arlington, VA
Duration: 25 Jun 200127 Jun 2001

Conference

ConferenceAmerican Control Conference
CityArlington, VA
Period25/06/0127/06/01

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Keywords

  • missile engineering
  • skid to turn missile
  • flight control
  • velocity control
  • aerodynamics

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