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Use of steepest descent and various approximations for efficient computation of minimum noise aircraft landing trajectories
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Witt, R. M. Cook, G. |
| Copyright Year | 1976 |
| Description | 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. |
| File Size | 2395188 |
| Page Count | 86 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760023831 |
| Archival Resource Key | ark:/13960/t5v747036 |
| Language | English |
| Publisher Date | 1976-08-01 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Approximation Aircraft Landing Computation Aircraft Noise Steepest Descent Method Wind Tunnel Tests Computerized Simulation Descent Trajectories Optimization Computer Programs Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |