FIELD: measuring equipment; cosmonautics.
SUBSTANCE: group of inventions relates to means of measuring the Earth's gravitational field (EGF) using a spacecraft (SC) in a circular orbit. Essence: device for measuring EGF contains a sensitive element of an accelerometer, a moment sensor, Thompson spinning top (2) installed in loaded state on fixed base (3) and fixed in guide (8) through bearing (10). Guide (8) is fixed on housing (1) of the device and in base (3) by means of springs (9). Thompson spinning top (2) is connected to electric motor (5) via electric coupling (4). Electric motor (5) and electric coupling (4) are connected to accumulator (7). At that, electric coupling (4) is connected to accumulator (7) through switch (6). A computer (12) connected to electric motor (5), accumulator (7) and strain gauge (11) is installed on housing (1). Strain gage (11) is installed between guide (8) and housing (1) of the device. Spacecraft is oriented along the normal to the EGF at the measurement section using the gravitational-magnetic orientation and stabilization system. Device for measuring EGF is installed in close proximity to the center of mass of the spacecraft and connected to the orientation and stabilization system. Thompson spinning top is brought into rotation. Gyroscopic moment arising at precession of Thompson spinning top is measured. Support reaction is determined by formula for gyroscopic moment of spinning top. Variation of normal reaction of the support is used to determine change in free fall acceleration and its distribution along the investigated section of the spacecraft trajectory. Based on the measurement of the free fall acceleration, the EGF force is determined at the measurement point.
EFFECT: higher accuracy and simplified EGF measurement.
2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
LASER SPACE GRAVITY GRADIOMETER | 2021 |
|
RU2754098C1 |
METHOD OF MEASURING ANOMALIES IN EARTH'S GRAVITATIONAL FIELD DURING LABORATORY OPERATIONS AND DEVICE FOR REALISING SAID METHOD | 2008 |
|
RU2398249C2 |
METHOD OF CONTROLLING MOVEMENT OF SPACECRAFT WITH CONTROLLED ORIENTATION | 2020 |
|
RU2767648C1 |
METHOD FOR DETERMINING FRICTION COEFFICIENT OF RUDDING PAIRS AND DEVICE FOR ITS IMPLEMENTATION | 2022 |
|
RU2785527C1 |
COMBINED GRAVITATIONAL ORIENTATION SYSTEM OF A SMALL SPACECRAFT | 2016 |
|
RU2658070C2 |
METHOD FOR DETECTING ANOMALIES OF GRAVITATION FIELD OF EARTH DURING LABORATORY SESSIONS | 2005 |
|
RU2308744C2 |
ASTRO-INERTIAL NAVIGATION SYSTEM WITH CORRECTION FOR THE EARTH'S GRAVITATIONAL FIELD | 2023 |
|
RU2820600C1 |
METHOD FOR DYNAMIC HIGH-ACCURACY ORIENTATION AND STABILIZATION OF SPACECRAFT | 2018 |
|
RU2702932C1 |
METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE | 2015 |
|
RU2594056C1 |
METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE | 2015 |
|
RU2594057C1 |
Authors
Dates
2024-08-21—Published
2023-11-14—Filed