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기술보고서

기술보고서 게시판 내용
타이틀	4D Dynamic Required Navigation Performance Final Report
저자	Finkelsztein, Daniel M.;; Sturdy, James L.;; Alaverdi, Omeed;; Hochwarth, Joachim K.
Keyword	AIR TRANSPORTATION;; AIRCRAFT CONFIGURATIONS;; AIRCRAFT MODELS;; AIRCRAFT PERFORMANCE;; ALGORITHMS;; AREA NAVIGATION;; AVIONICS;; CONTROL BOARDS;; DATA BASES;; INERTIAL NAVIGATION;; MATHEMATICAL MODELS;; TECHNOLOGY ASSESSMENT;; TRAJECTORIES
URL	http://hdl.handle.net/2060/20110007360
보고서번호	NASA/CR-2011-217051
발행년도	2011
출처	NTRS (NASA Technical Report Server)
ABSTRACT	New advanced four dimensional trajectory ƔDT) procedures under consideration for the Next Generation Air Transportation System (NextGen) require an aircraft to precisely navigate relative to a moving reference such as another aircraft. Examples are Self-Separation for enroute operations and Interval Management for in-trail and merging operations. The current construct of Required Navigation Performance (RNP), defined for fixed-reference-frame navigation, is not sufficiently specified to be applicable to defining performance levels of such air-to-air procedures. An extension of RNP to air-to-air navigation would enable these advanced procedures to be implemented with a specified level of performance. The objective of this research effort was to propose new 4D Dynamic RNP constructs that account for the dynamic spatial and temporal nature of Interval Management and Self-Separation, develop mathematical models of the Dynamic RNP constructs, "Required Self-Separation Performance" and "Required Interval Management Performance," and to analyze the performance characteristics of these air-to-air procedures using the newly developed models. This final report summarizes the activities led by Raytheon, in collaboration with GE Aviation and SAIC, and presents the results from this research effort to expand the RNP concept to a dynamic 4D frame of reference.