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Real-time optimization for use in a control allocation system to recover from pilot induced oscillations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Leonard, Michael W. |
| Copyright Year | 2013 |
| Description | Integration of the Control Allocation technique to recover from Pilot Induced Oscillations (CAPIO) System into the control system of a Short Takeoff and Landing Mobility Concept Vehicle simulation presents a challenge because the CAPIO formulation requires that constrained optimization problems be solved at the controller operating frequency. We present a solution that utilizes a modified version of the well-known L-BFGS-B solver. Despite the iterative nature of the solver, the method is seen to converge in real time with sufficient reliability to support three weeks of piloted runs at the NASA Ames Vertical Motion Simulator (VMS) facility. The results of the optimization are seen to be excellent in the vast majority of real-time frames. Deficiencies in the quality of the results in some frames are shown to be improvable with simple termination criteria adjustments, though more real-time optimization iterations would be required. |
| File Size | 228736 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20140008292 |
| Archival Resource Key | ark:/13960/t8ff8s34b |
| Language | English |
| Publisher Date | 2013-08-19 |
| Access Restriction | Open |
| Subject Keyword | Optimal Control Pilot Induced Oscillation Control System Design Controllers Vertical Motion Simulators Actuators Attitude Control Control Systems Design Control Stability Active Control Aircraft Control Real Time Operation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |