Optimal Command Generation for Tracking a Class of Discontinuous TrajectoriesSource: Journal of Dynamic Systems, Measurement, and Control:;1976:;volume( 098 ):;issue: 002::page 167Author:S. Weissenberger
DOI: 10.1115/1.3427005Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Commands are found to drive a linear system to optimally track a class of prescribed trajectories, each of which contains a point of discontinuity. The paper focuses on the guidance problem of command generation, to be implemented in a feedforward fashion; the necessary additional control or feedback regulation structure is not studied in detail, but assumed to be provided in applications as a conventional error-feedback regulator. Solutions are found for the infinite-time problem which are optimal with respect to a quadratic performance criterion; suboptimal controls which satisfy a continuity condition are also found. The controls have applications to certain problems in aircraft guidance where command trajectories are piecewise continuous. Several examples are worked out in detail, with comparisons with conventional, nonfeedforward solutions to the problem, and a brief discussion of a simpler, suboptimal solution.
keyword(s): Aircraft , Errors , Feedback , Feedforward control AND Linear systems ,
|
Show full item record
| contributor author | S. Weissenberger | |
| date accessioned | 2017-05-08T23:00:25Z | |
| date available | 2017-05-08T23:00:25Z | |
| date copyright | June, 1976 | |
| date issued | 1976 | |
| identifier issn | 0022-0434 | |
| identifier other | JDSMAA-26037#167_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/88491 | |
| description abstract | Commands are found to drive a linear system to optimally track a class of prescribed trajectories, each of which contains a point of discontinuity. The paper focuses on the guidance problem of command generation, to be implemented in a feedforward fashion; the necessary additional control or feedback regulation structure is not studied in detail, but assumed to be provided in applications as a conventional error-feedback regulator. Solutions are found for the infinite-time problem which are optimal with respect to a quadratic performance criterion; suboptimal controls which satisfy a continuity condition are also found. The controls have applications to certain problems in aircraft guidance where command trajectories are piecewise continuous. Several examples are worked out in detail, with comparisons with conventional, nonfeedforward solutions to the problem, and a brief discussion of a simpler, suboptimal solution. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Optimal Command Generation for Tracking a Class of Discontinuous Trajectories | |
| type | Journal Paper | |
| journal volume | 98 | |
| journal issue | 2 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.3427005 | |
| journal fristpage | 167 | |
| journal lastpage | 172 | |
| identifier eissn | 1528-9028 | |
| keywords | Aircraft | |
| keywords | Errors | |
| keywords | Feedback | |
| keywords | Feedforward control AND Linear systems | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;1976:;volume( 098 ):;issue: 002 | |
| contenttype | Fulltext |