| 54 |
Title |
TI |
[EN] Method for current regulation of permanently excited synchronous motors for guided missiles having an electromechanical actuating drive for the rudder |
| 71/73 |
Applicant/owner |
PA |
LFK GMBH, DE
|
| 72 |
Inventor |
IN |
FRENZEL BERNHARD, DE
;
KILGER FRIDBERT, DE
|
| 22/96 |
Application date |
AD |
Feb 20, 2001 |
| 21 |
Application number |
AN |
78566101 |
|
Country of application |
AC |
US |
|
Publication date |
PUB |
Sep 10, 2002 |
33
31
32 |
Priority data |
PRC
PRN
PRD |
DE
10007120
20000217
|
| 51 |
IPC main class |
ICM |
H02P 5/28
|
| 51 |
IPC secondary class |
ICS |
|
|
IPC additional class |
ICA |
|
|
IPC index class |
ICI |
|
|
Cooperative patent classification |
CPC |
H02P 6/28
|
|
MCD main class |
MCM |
|
|
MCD secondary class |
MCS |
H02P 6/28
(2016.01)
|
|
MCD additional class |
MCA |
|
| 57 |
Abstract |
AB |
[EN] In a method for current regulation of permanently excited synchronous motors for guided missiles with an electromechanical actuating drive for the rudder, the commanded current is always guided orthogonally to the magnet-wheel flow. Further:a) from measured current of two voltage phases, a measured magnitude of a current-space pointer is determined and an error value for the current is added to a desired value of the amount via a correction regulator; andb) from measured current of two voltage phases as well as from the angle command of the current-space pointer, a measurement for the angle error is determined and added to the desired angle value via a correction regulator.The method according to the invention can be implemented with little hardware expenditure and in a compact design size, even for high rotational speeds of >10,000 min-1. Current-regulating methods used heretofore, which involve frequency response compensation in polar coordinates, cannot be used with synchronous motors, i.e. explicit determination of the angle of the space-current pointer fails in cases where the measured current disappears. |
| 56 |
Cited documents identified in the search |
CT |
US000003642233A
US000003946691A
US000003972224A
US000004612488A
US000004683407A
US000004991429A
US000005649422A
US000005670856A
US000006075332A
US000006362590B2
|
| 56 |
Cited documents indicated by the applicant |
CT |
DE000019635847A1
|
| 56 |
Cited non-patent literature identified in the search |
CTNP |
|
| 56 |
Cited non-patent literature indicated by the applicant |
CTNP |
|
|
Citing documents |
|
Determine documents
|
|
Sequence listings |
|
|
|
Search file IPC |
ICP |
H02P 21/00 J
H02P 21/00
|
