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Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff

Effects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff - - Washington, D.C. NASA 1982 - 30 p. - NASA TP - 1978 : 1982 .

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Subjects--Topical Terms:

Magnetic leader cable, Aircraft guidance, Avionics, Aircraft control system

Universal Decimal Class. No.: LNASA TP - 1978 : 1982

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