Loading...
Please wait, while we are loading the content...
Analytical solutions to constrained hypersonic flight trajectories
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lu, Ping |
| Copyright Year | 1992 |
| Description | The flight trajectory of aerospace vehicles subject to a class of path constraints is considered. The constrained dynamics is shown to be a natural two-time-scale system. Asymptotic analytical solutions are obtained. Problems of trajectory optimization and guidance can be dramatically simplified with these solutions. Applications in trajectory design for an aerospace plane strongly support the theoretical development. |
| File Size | 614313 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930009413 |
| Archival Resource Key | ark:/13960/t8vb32c5h |
| Language | English |
| Publisher Date | 1992-11-30 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerospace Planes Aerospace Vehicles Trajectory Control Hypersonic Flight Flight Paths Spacecraft Guidance Cruising Flight Trajectory Analysis Asymptotic Methods Trajectory Optimization Ascent Trajectories Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
