- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- A method for determining the appropriate longitudinal and lateral decision height dispersion limits for any airplane/control system combination during an instrument landing approach is presented. An example is worked out to clarify the steps required. It is shown that the current longitudinal decision height dispersion limits are well suited for a DC-8 with the example control system, but that the lateral limits are too loose to guarantee acceptable touchdowns with the example system subjected to recommended wind and shear disturbances.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19720015001.
Accession ID: 72N22651.
- No Copyright.
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