FIELD: space engineering. SUBSTANCE: method is based on processing measurements of errors of gimballess attitude control system performed by means of astrosensors before and after each of three flat rotations of space vehicles performed about its body axis through angles aliquant to 360 deg, for example 90 deg or 180 deg. As a result, multiplicative error of gyro-inertial meters caused by errors of their scale factors and errors of position of sensitivity axes is estimated. EFFECT: enhanced efficiency. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR AUTOMATIC COMPENSATION OF STRAPDOWN ATTITUDE REFERENCE SYSTEM ERRORS IN SPACECRAFT ORIENTATION CONTROL SYSTEM AND APPARATUS REALISING SAID METHOD | 2012 |
|
RU2517018C2 |
| METHOD OF CORRECTING ANGULAR VELOCITY METERS OF SPACESHIP STRAPDOWN INERTIAL ORIENTATION SYSTEMS AND DEVICE TO THIS END | 2011 |
|
RU2466068C1 |
| METHOD FOR RAPID DETERMINATION OF ANGULAR ELEMENTS OF EXTERNAL ORIENTATION OF SPACE SCANNER PHOTOGRAPH | 2015 |
|
RU2597024C1 |
| CARDANLESS INERTIAL POSITIONING SYSTEM ELECTROSTATIC GYROSCOPES ERRORS CALIBRATION METHOD UNDER CONDITIONS OF ORBITAL SPACE CRAFT | 2018 |
|
RU2678959C1 |
| METHOD FOR CALIBRATING ANGULAR VELOCITY SENSORS OF GIMBALLESS INERTIA MEASUREMENT MODULE | 2010 |
|
RU2447404C2 |
| METHOD FOR CALIBRATING PARAMETERS OF PLATFORM-LESS INERTIAL MEASURING MODULE | 2004 |
|
RU2269813C2 |
| NAVIGATION COMPLEX, VELOCITY AND COORDINATES' CALCULATION, GIMBALLESS INERTIAL ATTITUDE-AND-HEADING REFERENCE SYSTEM, CORRECTION METHOD FOR INERTIAL TRANSDUCERS AND DEVICE FOR ITS IMPLEMENTATION | 2007 |
|
RU2373498C2 |
| CALIBRATION METHOD OF INERTIAL MEASUREMENT MODULE AS TO CHANNEL OF ACCELEROMETERS | 2011 |
|
RU2477864C1 |
| METHOD AND DEVICE FOR CONTROLLING MOTION OF A SPACECRAFT WITH CONTROLLED ORIENTATION | 2017 |
|
RU2669481C1 |
| ADAPTIVE STRAP DOWN INERTIAL ATTITUDE-AND-HEADING REFERENCE SYSTEM | 2016 |
|
RU2647205C2 |
