Optimum calibration and alignment filter gains for minimizing ballistic impact error
Optimum calibration and alignment filter gains for minimizing ballistic impact error
- Neue Suche nach: Grewal, M.S.
- Neue Suche nach: Henderson, V.D.
- Neue Suche nach: Grewal, M.S.
- Neue Suche nach: Henderson, V.D.
The objective of this paper is to show that minimizing the trace of the calibration and alignment error covariance matrix of an inertial ballistic guidance system also minimizes circular error probable (CEP) at the time of impact, independent of in-flight error miss-coefficients. This paper gives a complete derivation of the optimum calibration and alignment gains which minimize the error covariance matrix trace, and then follows with the derivation for minimizing the trace of the impact error covariance matrix. The two are shown to be equivalent.
Dokumentinformationen
Optimum calibration and alignment filter gains for minimizing ballistic impact error
Die optimalen Verstaerkungen der Eichung- und Justierungsfilter zur Minimierung des ballistischen Stossfehlers
Proc. of the 1986 American Control Conf. ; 3 ; 1574-1575
1986
2 Seiten, 5 Quellen
Aufsatz (Konferenz)
Englisch
Ähnliche Titel
Airdata calibration using error state filter
| AIAA | 2017
Calibration Fluid Spec gains International Status
| Kraftfahrwesen | 1978