The following areas related to landing trajectory optimization research were discussed: (1) programming and modifying the steepest descent optimization procedure, (2) successfully iterating toward the optimum for a four-mile trajectory, (3) beginning optimization runs for a twenty-mile trajectory, and (4) adapt wind tunnel data for computer usage. Other related areas were discussed in detail in the two previous annual reports.
Use of steepest descent and various approximations for efficient computation of minimum noise aircraft landing trajectories
1976-08-01
Report
No indication
English
Minimum noise impact aircraft trajectories
Elsevier | 1984
A General Steepest Descent Algorithm
IEEE | 1976
|Methodology for multiaircraft minimum noise impact landing trajectories
Tema Archive | 1982
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