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Designing low bandwidth propulsive-only flight controllers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Biezad, Daniel J. Azzano, Christopher P. |
| Copyright Year | 1996 |
| Description | Results from an investigation of using engine commands to control flight attitude are described. In-flight operation with simulated failed flight controls is reviewed and ground simulations of piloted propulsive-only control to touchdown are analyzed. A design of an optimal control law to assist the pilot is presented. Recommendations are made for more robust design and implementation. Results to date indicate that simply and effective augmented control can be achieved in a wide variety of failed configurations. |
| File Size | 500364 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19960054271 |
| Archival Resource Key | ark:/13960/t6644p821 |
| Language | English |
| Publisher Date | 1996-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Attitude Inclination Control Simulation Optimal Control Bandwidth Engine Control Control Theory Flight Control Propulsion System Configurations Dynamical Systems Linear Quadratic Regulator Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
