FIELD: astronautics.
SUBSTANCE: invention relates to rocket engineering. Device for determination of spatial orientation of Soyuz-2 space rocket, with installed on-board standard units of navigation equipment of consumer and triaxial gyrostabilizer, comprises unit of angular speeds sensors, which inputs are directly connected to on-board digital computer. Unit of angular velocity sensors includes a unit of sensitive elements consisting of at least three accelerometers.
EFFECT: higher accuracy of orientation.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| THRUST CONTROL DEVICE FOR THE PROPULSION SYSTEMS OF THE SOYUZ-2 AND ANGARA SPACE ROCKETS, BASED ON THE ASSESSMENT OF THE CURRENT VALUES OF THRUST DURING FLIGHT ACCORDING TO TELEMETRIC INFORMATION FOR FALLING SEPARABLE PARTS INTO A GIVEN AREA | 2022 |
|
RU2793861C1 |
| METHOD OF AUTONOMOUS NAVIGATION FOR SPACE OBJECT | 2018 |
|
RU2727784C2 |
| DEVICE FOR ASSESSING POSSIBILITY OF LAUNCHING SOYUZ-2 SPACE ROCKET BASED ON WEATHER SURVEY RESULTS | 2019 |
|
RU2726582C1 |
| AUTONOMOUS COMPLEX FOR CORRECTION OF INERTIAL SYSTEMS OF PLATFORM ORIENTATION AND NAVIGATION OF MOBILE OBJECTS | 2022 |
|
RU2826826C2 |
| METHOD FOR DETERMINING ANGULAR ORIENTATION OF GROUND VEHICLE | 2019 |
|
RU2723976C1 |
| METHOD OF THREE-AXIS GYROSTABILIZER STABILIZED PLATFORM INDEPENDENT INITIAL ALIGNMENT IN HORIZONTAL PLANE AND AT SPECIFIED AZIMUTH | 2015 |
|
RU2608337C1 |
| SATELLITE GRAVITY GRADIOMETRY METHOD | 2020 |
|
RU2745364C1 |
| AIRCRAFT CONTROL DEVICE SUITABLE FOR POSITION INDICATION UPON INCURRENCE OFF-NOMINAL (EMERGENCY) SITUATION | 2016 |
|
RU2632559C2 |
| METHOD OF ONBOARD CONTROL IN ROCKET FLIGHT EMERGENT TERMINATION | 2011 |
|
RU2476357C2 |
| METHOD OF INDEPENDENT AZIMUTHAL ORIENTATION OF PLATFORM OF THREE-AXIS GYROSTABILISER ON MOVABLE BASE | 2013 |
|
RU2541710C1 |
