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Air Traffic Management Concept Baseline Definition - The Boeing ...

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function of all the ICPs of elements between the users (i.e., communications elements<br />

between a pilot and a controller). Once ICP T is determined, it can be compared against a<br />

specific RCP to determine if the RCP is met.<br />

Determination of ICP T is part of the process of gaining operational approval for the given<br />

RCP airspace or operation. ICP is inherently tied to one or more specific technologies. It<br />

is the term used to describe the performance of the particular communication path as<br />

certified by the cognizant authority. ICP can be associated with a given aircraft because it<br />

is strongly influenced by the aircraft’s equipage and the communication support<br />

arrangements that have been made for it.<br />

5.1.2.3 Actual Communication Performance<br />

Actual communication performance (ACP) is an observation of the dynamic operational<br />

communication capability of the same communication elements as was used for the<br />

determination of ICP. ACP is expressed in the same terms and parameters as are RCP and<br />

ICP, but at a given instant may differ from the ICP of a particular path. ACP can be<br />

determined by monitoring the communication path or by monitoring the current condition<br />

of the elements of the path. It is recognized that various cognizant authorities may wish to<br />

specify the necessary reactions of the airspace manager and flight crew when ACP differs<br />

from ICP.<br />

5.1.3 Navigation Performance<br />

<strong>Air</strong>plane navigation requirements for each phase of flight are a function of airplane<br />

separation requirements. <strong>The</strong> separation of aircraft and obstacles also provides<br />

requirements especially in the approach/landing phase. A high degree of confidence in the<br />

aircraft staying within a specified volume of airspace is needed to establish separation<br />

standards. <strong>The</strong> dimensions of this volume are based on the probability of the aircraft<br />

navigation system performance not exceeding a specified error. However, airplane<br />

separation criteria established by the FAA also account for the availability and limitations<br />

of communications, and surveillance services, as well as operational factors (e.g., the<br />

crew/autopilot’s use of the navigation information to control the airplane position) in<br />

addition to navigation requirements.<br />

<strong>The</strong> increased equipment accuracy and world wide coverage of new systems based on<br />

Global Positioning System (GPS) navigation will greatly improve operations because of<br />

the performance limitations of ground aids. This is achieved in large part by providing<br />

increased integrity monitoring and more reliability. As navigation evolves to satellite based<br />

aids, consideration of additional failure modes will have to be considered. <strong>The</strong>se and<br />

potentially more sophisticated crew alerting schemes will keep driving new requirements<br />

as applications evolve. Cost considerations may become driving factors, but minimizing<br />

the impact on crew interfaces as a fundamental design philosophy will help as will the<br />

potential use of navigation technology developed for the mass market.<br />

RTCA’s document DO-236, “Minimum Aviation System Performance Standards:<br />

Required Navigation Performance for Area Navigation” (RTCA, 1997) establishes the<br />

requirements for the airborne navigation component of the CNS/ATM operating<br />

57

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