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Extensions to pifcgt: multirate output feedback and optimal disturbance suppression
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Broussard, J. R. |
| Copyright Year | 1986 |
| Description | New control synthesis procedures for digital flight control systems were developed. The theoretical developments are the solution to the problem of optimal disturbance suppression in the presence of windshear. Control synthesis is accomplished using a linear quadratic cost function, the command generator tracker for trajectory following and the proportional-integral-filter control structure for practical implementation. Extensions are made to the optimal output feedback algorithm for computing feedback gains so that the multirate and optimal disturbance control designs are computed and compared for the advanced transport operating system (ATOPS). The performance of the designs is demonstrated by closed-loop poles, frequency domain multiinput sigma and eigenvalue plots and detailed nonlinear 6-DOF aircraft simulations in the terminal area in the presence of windshear. |
| File Size | 2620103 |
| Page Count | 127 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860013110 |
| Archival Resource Key | ark:/13960/t2v45mb5q |
| Language | English |
| Publisher Date | 1986-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Performance Tests Digital Systems Control Systems Design Computerized Simulation Feedback Control Flight Control Design Analysis Adjusting Digital Navigation Algorithms Computation Optimal Control Eigenvalues Wind Shear 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 |