This paper describes work demonstrating the feasibility of using a pre-compensator in a co mpressor- turbine refrigeration system for aircraft cabin cooling to permit largely independent closed- loop control of cooling air temperature and drive shaft speed.
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References
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Kurylowich, G. and Lloyd, A.J.P.1982. 'Aircraft vehicle improvements via microprocessors ', SAE Technical Paper Series 820868.
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Rosenbrock, H.H.1974. Computer-aided control systems design, Academic Press.
