RussianPatents.com

Board for selecting observation objects from orbital spacecraft

Board for selecting observation objects from orbital spacecraft
IPC classes for russian patent Board for selecting observation objects from orbital spacecraft (RU 2482451):
G01C21/24 - specially adapted for cosmonautical navigation
Another patents in same IPC classes:
Method for ephemeral provisioning of process for controlling global navigation satellite system spacecraft Method for ephemeral provisioning of process for controlling global navigation satellite system spacecraft / 2477836
Invention can be used for ephemeral provisioning of a process for controlling global navigation satellite system (GNSS) spacecraft. A low-orbiting spacecraft fitted with apparatus for synchronising the on-board time scale with the system time scale, apparatus for determining orbit parameters from ground-based radio beacons and consumer navigation equipment is taken to an orbit. During orbit flight thereof, the on-board time scale is synchronised with the system time scale of the GNSS; orbit parameters are determined from radio beacon signals; a GNSS spacecraft navigation message signal is received; Doppler frequency shift of the message signal is measured. Orbit parameters of the low-orbiting spacecraft and the measured values of the Doppler frequency shift of the message signal on-board the low-orbiting spacecraft are used to determine the orbit of navigation GNSS spacecraft and then transmitted for reception thereof at the GNSS spacecraft.
Method of monitoring continuity of navigation field of global navigation satellite system Method of monitoring continuity of navigation field of global navigation satellite system / 2477835
Invention can be used for rapid monitoring of continuity of the navigation field of the global navigation satellite system (GNSS). Continuity if monitored on a low-orbiting spacecraft fitted with consumer navigation apparatus. During orbital flight, navigation messages of visible GNSS spacecraft are continuously received; navigational sighting is carried out; some of the received navigation messages are used and several sets of consumer coordinates are obtained. By processing redundant navigation information, the quality of navigation signals of all visible GNSS spacecraft are analysed. Upon detection of malfunction of a certain GNSS spacecraft, a fault feature is rapidly generated and transmitted, which is received in on-board control systems of the GNSS spacecraft and the fault feature is entered into the system log.
Device to select objects of surveillance from orbital spacecraft Device to select objects of surveillance from orbital spacecraft / 2471150
Device comprises a globe with a planet surface map applied on it, a spiral element that models an orbit of a spacecraft (SC), a facility to lock the spiral element on the axis of globe rotation. The spiral element is arranged in the form of an orbit turn with a positive incline of the SC. The start of the orbit turn shall be a point of the orbit located beyond the quarter of the SC circulation period to the ascending unit of the orbit. The end of the orbit turn shall be a point of the orbit that is distant by the quarter of the SC circulation period after the next ascending unit of the orbit. The facility for fixation of the spiral element on the axis of globe rotation is arranged in the form of two connection elements, the angular size of every of which, measured from the centre of the globe, is equal to 90°-i, where i - orbit inclination.
Angle measurement device Angle measurement device / 2470258
Angle measurement device comprises a lens hood, a channel of a non-detuned geometric reference in the form of a lighting unit, a unit of a beam divider, a flat mirror installed on a basic plane and a non-detuned mirror-prism unit, a lens, a photodetector and a computing unit. The beam divider unit - an optical element glued from a lens and mirror-lens system, in the area of gluing producing an inclined beam-dividing face, in which: the first input surface is arranged in the lens system and is arranged as flat with a dot diaphragm applied on it; the second output surface is arranged in the mirror-lens system is arranged as flat with an adhered plano-convex lens with a mirror spherical surface, at the same time the second surface is input for radiation reflected with the mirror spherical surface; the third output surface is arranged in the mirror-lens system, is arranged in the form of a concave spherical surface, the front focus point of which is matched with the image of the dot diaphragm from the mirror spherical surface, at the same time the third surface is also an input surface for radiation reflected with a flat mirror; the fourth output surface in the lens system is a convex spherical surface. For radiation reflected with a flat mirror, the third and fourth surfaces operate as a telescopic system with angular magnitude of 0.5x.
Board for selecting observation objects from orbital spacecraft Board for selecting observation objects from orbital spacecraft / 2469274
Board for selecting a ground surveillance object from an orbital spacecraft refers to space engineering. The board for selecting ground surveillance objects from an orbital spacecraft has a flexible belt with a map of the surface of the plane, a semitransparent plate placed on top and a device for enabling movement of the belt with the map along the semitransparent plate from two shafts spaced apart and mounted parallel each other. The semitransparent plate consists of two parts. One edge of the first part of the semitransparent plate is curvilinear and has the shape of the curved line of the orbit of the spacecraft between ascending and descending nodes and the other edge is directed along the equator line of the map. One edge of the second part of the semitransparent plate is curvilinear and has the shape of the curved line of the orbit of the spacecraft between ascending and descending nodes and the other edge is directed along the latitude line of the map. Both parts of the semitransparent plate are mounted with superposition of the outermost points of the curvilinear edge of one part of the semitransparent plate with the outermost points of the curvilinear edge of the other part of the semitransparent plate and with possibility of each part of the semitransparent plate turning about an axis directed along the equator line of the map.
Angle measurement device Angle measurement device / 2469266
Device comprises a lens, a matrix photodetector device (PDD), a calculation unit and a channel of a geometric reference in the form of a lighting unit, a collimator unit and a mirror-prism unit that introduces radiation from the lighting unit into the lens. The lighting unit is arranged in the form of three sources of light installed in front of input diaphragms and arranged at the angle of 120° to each other. The collimator unit is arranged in the form of three input and three output point diaphragms arranged on the rear face of the mirror-prism unit, which faces the lens, outside its inlet pupil, and is rigidly connected to the support surface of the device. The mirror-prism unit is a single monoblock in the form of parallel smaller front and larger rear hexagonal faces, adjacent ribs of which are arranged at the angle of 120° to each other and form six side mirror faces. The front face is arranged as capable of reflecting rays developed by a lighting unit and input holes of the collimator unit. The lens on the sensitive site of the PDD generates dot element images of the geometric reference channel, and additionally dot element images received from beams reflected by the front face of the mirror-prism unit.
Weapon orientation method Weapon orientation method / 2466343
Measuring device and calculation and indication unit are installed on the weapon. Measurement of the measuring device data, calculation of current values of azimuth angle and elevation angle of weapon in the calculation and indication unit, indication of values of azimuth angle and elevation angle and turning of weapon to the required values of guidance angles as to azimuth and elevation is performed. Measuring device is represented with two-antenna satellite navigation system installed on the weapon parallel to weapon axis of sight with guidance of antennae to upper hemisphere. Measurement of coordinates of antenna location is performed with frequency of not less than 1 Hz. Calculation in calculation and indication unit is carried out as per measured antenna location coordinates.
Board for selecting observation objects from orbital spacecraft Board for selecting observation objects from orbital spacecraft / 2463559
Board for selecting observation objects from orbital spacecraft includes a plate with a map of the earth's surface, a semitransparent plate placed on top of the map of the planet, and means of facilitating displacement of the semitransparent plate along the equatorial line on the map. One edge of the semitransparent plate is curvilinear and has the shape of the curved line of the path of the orbit pass of the spacecraft. The semitransparent plate is placed with superposition of points of said curvilinear edge of the plate, which simulate node points, with the equatorial line on the map of the planet and with location of the edge of the plate, opposite said curvilinear edge of the plate, over one of said hemispheres of the map of the planet. There is a means of facilitating displacement of the semitransparent plate to a position where the edge of the plate, opposite said curvilinear edge of the plate, lies over the other of the hemispheres of the map of the planet with superposition of points of said curvilinear edge of the plate, which simulate node points, with the equatorial line on the map of the planet. The technical result is achieved through the proposed changes to the shape and size of the semitransparent plate, the proposed installation of the semitransparent plate and introduction into the board of the proposed means of facilitating displacement of the semitransparent plate to a new proposed position.
Method of determining ephemeral information in user equipment and apparatus for realising said method Method of determining ephemeral information in user equipment and apparatus for realising said method / 2460970
During flight of spacecraft in the visibility range of control and measurement stations (CMS), pseudorange to the CMS is measured on navigation radio signals of unmanned spacecraft based on the signal time delay. Doppler shift is determined and the measurements are transmitted to the computation centre of the main CMS. Based on the obtained values of predicted coordinates at fixed reference time instants with a defined interval, ephemerides are determined, which are then loaded onto the unmanned spacecraft using transmitting antennae of the CMS network, and then sent to users in form of a navigation message. Knowing matched ephemerides of the unmanned spacecraft at reference time instants, the user determines the coordinates of the unmanned spacecraft at an arbitrary moment in time by integrating equations of the model of the motion of the unmanned spacecraft.
Device for recording particles of space garbage and micrometeoroids Device for recording particles of space garbage and micrometeoroids / 2454628
Device for recording particles of space garbage and micrometeoroids consists of two or three video cameras equally located in the space through the base length. Video cameras are mounted along one line and blocks with solar batteries, objective lenses with charge-coupled device matrixes and blends. Blocks are connected to each other by means of a moving telescopic rod about which a cylinder in the form of metal-dielectric-metal film structure is located. In one of the optic blocks there installed is bottle with chemical hardener; each of optic blocks is equipped with magnetic control system in the form of one magnetometer and three electromagnets, as well as solar sensor, GPS-receiver, photodiodes located on side surfaces and onboard computer.
Sun angular coordinate indicator Sun angular coordinate indicator / 2244263
Device has optical spectrum filter, slit mask, multi-element photo-sensitive detector, threshold elements, photo-detector register, counter, output register, clock pulse generator. Multi-element photo-sensitive detector consists of elementary photo-detectors placed behind one another along quadratic curve. Normal lines to sensitive areas of each elementary photo-detector and quadratic curve lie in same plane.
Method of orientation of spacecraft Method of orientation of spacecraft / 2247945
Proposed method includes measurement of angles of position of optical axes of astro-visual units tracking the stars relative to body-axis coordinate system. For determination of orientation of mobile object, use is made of coordinates of its center of mass in geocentric coordinate system which are determined by means of high-precision global navigation satellite system.
Method for determining angles of orientation of moving object and device for realization of method Method for determining angles of orientation of moving object and device for realization of method / 2273826
Satellite navigation equipment and three gyro-integrators simultaneously determine values of projections of speed vector in starting and connected coordinates system respectively and transfer determined values to onboard digital computing machine, which, using received information, determines values of angles of orientation of moving object in space in accordance to algorithm for determining orientation of moving object.
Method of determining initial position of inertia block with respect to base coordinate system Method of determining initial position of inertia block with respect to base coordinate system / 2279635
Method comprises autonomous determination of the position of the instrument with respect to the horizontal plane coordinate system from the signals from the accelerometers and vector conforming of the coordinate systems for determining the position of the instrument coordinate system in azimuth.
Method of spatial orientation and stabilization / 2282154
Method comprises determining the vector of velocity of the object in a Cartesian coordinate system, determining integral characteristics of the variation of the velocity vector as a function of the direction of motion of the object in the space, and stabilizing the trajectory of motion of the movable object on the basis of the estimations depending on the direction chosen from the stars sky.
Device for determining vertical of spacecraft location Device for determining vertical of spacecraft location / 2282155
Device comprises two spheres mounted with a spaced relation one to the other. The outer sphere is made of a superconducting material, and the inner sphere is made of a magnetic material. The outer sphere is secured to the spacecraft, and the inner sphere is shifted with respect to the center of gravity and has the radiation source. The output of the radiation receiving unit is connected with the information input of the recording unit whose control input is connected with the output of the board control unit.
Method of autonomous measurement of angular speed vector Method of autonomous measurement of angular speed vector / 2282826
Method can be used in moving objects' spatial orientation systems. Before beginning of movement of object, the coordinate system is chosen being comfortable for observer. Three stars are selected, along directions of which stars the speeds have to be measured and their angular coordinates are measured. After movement starts, current values of linear velocity are measured on the base of directions of navigating stars. Changes in linear velocity are calculated from directions of navigating stars, which are changes are caused by rotation of object, and basic components of angular speed vector are determined from directions of navigating stars.
Sun attitude pickup Sun attitude pickup / 2308005
The Sun attitude pickup has an optical system made in the form of a wide-angle lens including an inlet and outlet plano-convex lenses with a diaphragm placed between them, an optical element is positioned in its holes, matrix photodetector, and a unit for processing of information and computation of coordinates. The refractive indices of the optical components are selected proceeding from the relation: n1≥n2<n3, where n1 - the refractive index of the inlet plano-convex lens; n2 - the refractive index of the optical element; n3 - the refractive index of the outlet plano-convex lens.
Method for autonomous navigation and orientation of spacecrafts Method for autonomous navigation and orientation of spacecrafts / 2318188
Method for autonomous navigation and orientation of spacecrafts includes computer calculation of position in three-dimensional space of ort of radius-vector of support (calculated, a priori assumed) orbit, rigid attachment of optical-electronic device on the body of spacecraft and measurement of coordinates and brightness of stars, which are in the field of view during navigational sessions, in it.
Coherent transponder of phase synchronization Coherent transponder of phase synchronization / 2319931
Coherent transponder of phase synchronization has a radio receiving set, a radio transmitting set, an airborne standard of frequency (H-maser) and also a logic and commutation block. The radio transmitting so as the radio receiving set consists of two half-sets. The radio receiving set has a radio receiver module of the amplifier of a very high frequency, a preliminary amplifier of intermediate frequencies, a block of phase automatic adjustment of the frequency, the amplifier of the reference signal 2▾ and the secondary source of feeding.▾- nominal frequency. The coherent transponder of the phase synchronization provides transformation of the input signal in diapason 961▾ into an answer signal in the diapason 1120▾ used for synchronization of the airborne thermostating controlled generator. For reducing the drift of the phase of the answer signal the system of transformations of frequencies is built on the principle of complete matching of tracts of multiplying of the radio transmitting set and the heterodynes of the radio receiving set.

FIELD: physics.

SUBSTANCE: invention can be used to determine and select observation objects onboard an orbital spacecraft moving on a near-circular orbit. The board for selecting observation objects from an orbital spacecraft has a flexible tape with a map of the earth's surface, a semitransparent plate placed over said tape having an image of half the orbit pass of the spacecraft between ascending and descending nodes, and a device for moving the tape along the plate with two rollers spaced apart and mounted parallel to each other. The tape is stretched onto the rollers with possibility of movement thereof along the equator line. The map of the earth's surface is divided into two parts on the equator line. Part of the map with the image of the northern hemisphere and part of the map with the image of the southern hemisphere are arranged in series on the tape. The equator line of the part of the map with the image of the northern hemisphere is a continuation of the equator line of the part of the map with the image of the southern hemisphere. The device for moving the tape along the plate has processor rollers placed in parallel between the first and second rollers. The tape is stretched onto said rollers and the newly introduced process rollers. The size of the tape and the plates along the direction perpendicular to the equator is equal to the length of the latitude line of the map showing one of the hemispheres.

EFFECT: smaller size of the board.

3 dwg

 

The invention relates to the field of space technology and can be used to identify and select objects on Board an orbiting SPACECRAFT), moving in a near-circular orbit.

Known maps of the earth's surface (Votyakov A.A. Theoretical geography-3. Map of a flat earth. - M.: Sofia, 2002) and maps of the sky (celestial Map with the zodiac constellations. - M: DI EM BI, 2004), which can be used to identify and select geophysical and astronomical objects for observations performed with the AC. The lack of maps is that they do not have graphical information about the orbit of the SPACECRAFT.

The closest analogues adopted for the prototype, is the tablet to select the ground object observations from orbiting spacecraft (RF patent No. 2324898 from 26.01.2006. IPC G01C 21/24, B64G 1/22 - prototype)containing a flexible tape with a map of the earth's surface, installed over her translucent plate with the image of the two halves of the spiral orbit of the spacecraft, made with a combination of ascending node of the orbit starting the first half revolution of the orbit, and the descending node of the orbit starting the second half revolution of the orbit, and the device providing movement of the tape with the card along the plate with the image of the revolution orbit of the two raznesenii and bonded in parallel between the shafts, when this card is printed on the tape with a combination of start points and end the equator of the map, and the tape is made of a closed ring and stretched over the shaft with a circular movement along the equator line cards, and the distance between the axes of the shafts and the size of the plate with the image of the spiral orbit along the equator is made equal to the value (L-d)/2, where L is the length of the equator of the map; d is the absolute value of the inter-turn distance, measured in linear units along the equator of the map, and the radius of the shaft is made equal to the value of d/(2π).

When using the tablet moves the tape with the card along the plate, in turn combine point of the ascending and descending node of the orbit points of the equator of the map corresponding to the longitude of the ascending and descending nodes of the considered loop. Applied to the plate line orbit show on the map the route of the considered loop that allows you to identify and select objects on the earth's surface to be monitored from the SPACECRAFT.

Tablet, taken as the prototype, has the disadvantage tablet size is large enough and can create difficulties during its operational use (for example, aboard manned SPACECRAFT).

The task of the proposed device is improved ergonomic characteristics of the tablet to select objects on earth observations orbital is about the SPACECRAFT by reducing the size of the tablet.

The technical result is achieved by the fact that in the tablet to select objects on earth observations from orbiting spacecraft, including a flexible tape with a map of the earth's surface, installed over it semi-transparent plate with a picture of a half revolution of the orbit of the spacecraft between the ascending and descending nodes of the orbit and the device providing movement of the tape across the plate with two spaced and bonded in parallel between the shafts, while the tape is tight on the shaft can move along the line of the equator, optionally map the earth's surface is divided by the equator into two parts, and on the tape sequentially placed part of the map depicting the Northern hemisphere and part of a map depicting the southern hemisphere, the equator line of the map depicting the Northern hemisphere continues the line of the equator of the map with the image of the southern hemisphere, with the device providing movement of the tape along the plate introduced technological shafts placed in parallel between the first and second shafts, and the tape is stretched to the above-mentioned shafts and the newly introduced technological shafts, and the size of the tape and the plate along the direction perpendicular to the equator, equal to the length of the lines of latitude of the map, showing one of the hemispheres.

Figure 1 is an illustration of a layout on the ribbon parts of a map showing the Northern and southern hemispheres. In figure 2, 3 shows a possible circuit implementation of the proposed tablet.

In figure 1, 2, 3 indicated:

1 - ribbon;

2 - part map of the Northern hemisphere;

3 - part cards with the image of the southern hemisphere;

4 - line of the equator of the map depicting the Northern hemisphere;

5 - the equator line of the card with the image of the southern hemisphere;

6 - the starting point of the line of the equator of the map depicting the Northern hemisphere;

7 is an end point of the line of the equator of the map depicting the Northern hemisphere;

8 - the starting point of the line of the equator of the map with the image of the southern hemisphere;

9 is an end point of the line of the equator of the map with the image of the southern hemisphere;

10 is a semi - transparent plate;

11 - line orbit;

12 - point ascending node of the orbit;

13 - point of the descending node of the orbit;

14, the first and second shafts;

15 technological shafts;

16 is a structural member that connects the axis of the shafts;

17 - element design, the locking position of the plate over the shaft.

Map the earth's surface is divided by the equator into two parts: on one side of the map shows the Northern hemisphere of the earth surface on the other side of the map shows the southern hemisphere the earth's surface. On a flexible tape 1 sequentially placed part of the map depicting the Northern hemisphere 2 and the part of the map with the image of the southern hemisphere 3.

Figure 1 presents an example of possible placement on the ribbon 1 two parts of a map with images of the southern and Northern hemispheres, 2 and 3. In the present example, each of the card 2 and 3, placed the image of the corresponding hemisphere with long continuous image of the hemisphere along the line of longitude expressed in degrees, is equal to 360°÷180°=540°. In this case, the card with the image of each hemisphere contains the image of one full hemisphere (for example, the image in the range of longitudes of 0°÷360°) and the image of the half hemisphere (e.g., in the range of longitudes of 0°÷180°or in the range of longitudes "-180°÷360°"-which are continuous with one another. Namely, the image in the range of longitudes of 0°÷360°" continues the image in the range of longitudes of 0°÷180°, forming a total continuous image in the range of longitudes of 0°÷540°". The image in the range of longitudes "-180°÷0°" continues the image in the range of longitudes of 0°÷360°, forming a total continuous image in the range of longitudes "-180°÷360°". As an example, figure 1 shows the case when part of the map depicting the Northern hemisphere 2 contains an image of the Northern hemisphere in the range of longitudes of 0°÷540°", and some cards with the image the receiving of the southern hemisphere 3 contains an image of the southern hemisphere in the range of longitudes"-180°÷360°".

The equator line of the map depicting the Northern hemisphere 4 and the equator line of the card with the image of the southern hemisphere 5 continue one another (lie on the same line, which line placement equatoral two parts of the map). Thus, for example, the end point of the line of the equator of the map depicting the Northern hemisphere 7 combined end point of the line of the equator of the map with the image of the southern hemisphere 9.

Above the ribbon 1 is set to semi-transparent plate 10.

The plate 10 is placed on line orbit 11 between adjacent ascending node of the orbit 12 and the descending node of the orbit 13.

The tablet contains a device providing movement of the tape 1 along the plate 10 which has mounted parallel to the first and second shafts 14 and technological shaft 15, mounted in parallel between the first and second shafts 14. The belt 1 is stretched to the shafts 14, 15 can move along the lines of equatoral cards 4, 5.

The size of the plate 10 along the lines of equatoral cards 4, 5 is equal to the length of the projection line of the orbit 11 on the equator and is calculated by the formula

where L is the length of the line of the equator in the longitude interval of 0°÷360°", measured in linear units; d is the absolute value of the inter-turn distance, measured in linear units along the line of the equator.

The size of the tape 1 and the plate 10 along the direction of the Department, perpendicular to the equator, equal to the length S of the line of latitude of the map, showing one hemisphere.

The device providing movement of the tape 1 along the plate 10 may include a structural member connecting the axis of the shafts 16 and the structural member, the locking position of the plate on the shaft, 17.

A structural member that connects the axis of the shafts 16, connects the axes of the shafts 14, 15 between itself and fixes the relative distance between the axes of the shafts 14, 15.

The structural member, the locking position of the plate on the shaft, 17, fixation of the position of the plate 10 above the shaft 14.

Figure 2 presents the realization of a device for providing movement of the tape 1 along the plate 10, in which the shafts 14, 15 tight tape 1 made of closed. Figure 3 presents the realization of a device for providing movement of the tape 1 along the plate 10, in which the shafts 14, 15 tight tape 1, the ends of which are fixed on technological shafts 15.

Working with the tablet as follows.

We believe that the coils of the orbit, count (start) from the ascending node of the orbit.

Rotation of the shafts 14, 15 and moves the tape 1 with respect to the plate 10 until the setting point of the line of the equator of the map depicting the Northern hemisphere 4, the longitude of which is equal to the value of the longitude of the ascending node of the considered orbits about the bits, with the point of the ascending node of the orbit 12. Line orbit 11 will show on the side of the map depicting the Northern hemisphere 2 the first half of the considered orbits orbits (solid line 11 in figure 1).

Rotation of the shafts 14, 15 and moves the tape 1 with respect to the plate 10 until the setting point of the line of the equator of the map with the image of the southern hemisphere 5, the longitude of which is equal to the value of the longitude of ascending node of the loop, the next question turn orbit, with the point of the ascending node of the orbit 12. Line orbit 11 will show on the map with the image of the southern hemisphere 3 route the second half of the considered orbits orbits (dotted line 11 in figure 1).

Thus, the line of the orbit 11 shows two parts of a map with images of the Northern and southern hemispheres 2 and 3 both parts of the route in question orbits orbit.

In the example images hemispheres intervals of longitude images hemispheres selected so that when both of the above builds, runs halves of orbits orbit, the user can directly use the values of the longitudes of the ascending nodes of the orbits of the orbit, defined in the interval"0°÷360°".

In General, images of the Northern and southern hemispheres can be performed in any interval of longitude, covering a full hemisphere, i.e. the distance between the end points of the intervals in the and longitude is equal to or more than 360°. For example, the minimum image of each hemisphere can be done in one of two intervals of longitude: "0°÷360°or -180°÷180°corresponding to the two common scales of reference longitude. Presented in the example in figure 1 image of the hemispheres, each of which contains the image of one and a half full hemisphere, can be regarded as the maximum meaningful picture of the hemispheres: the use of larger images hemispheres does not give any new features to the tablet, thus complicating the tablet due to the elongation of the tape.

Describe the technical effect of the invention.

The size of the tablet in the direction perpendicular to the equator, characterized by the size in the direction of the tape and the plate with the image of the orbit. In the tablet-prototype this is the length of the lines of latitude maps of the earth's surface equal to the value of 2*S. In the proposed tablet size tape 1 and the plate 10 in the direction perpendicular to the equator, equal to the value of S, i.e. twice less than in the tablet prototype. Thus, the proposed device improves ergonomics of the tablet to select objects on earth observations from orbiting SPACECRAFT by reducing the size of the tablet on the tablet prototype in two times.

The technical result is achieved accounts the proposed local images of the Northern and southern hemispheres on a flexible tape 1, and also due to the introduction of the device providing movement of the tape 1 along the plate 10 technological shafts 15, which stretched the tape 1, and the proposed size of the tape 1 and the plate 10.

The tablet to select objects observations from orbiting spacecraft, including a flexible tape with a map of the earth's surface, installed over it semi-transparent plate with a picture of a half revolution of the orbit of the spacecraft between the ascending and descending nodes of the orbit and the device providing movement of the tape across the plate with two spaced and bonded in parallel between the shafts, while the tape is tight on the shaft can move along the line of the equator, characterized in that map the earth's surface is divided by the equator into two parts and on the tape sequentially placed part of the map depicting the Northern hemisphere and part of the card with the image of the southern hemisphere while the equator line of the map depicting the Northern hemisphere is a continuation of the line of the equator of the map with the image of the southern hemisphere, with the device providing movement of the tape along the plate introduced technological shafts placed in parallel between the first and second shafts, and the tape is stretched to the above-mentioned shafts and the newly introduced technology is Aly, and the size of the tape and the plate along the direction perpendicular to the equator, equal to the length of the lines of latitude of the map, showing one of the hemispheres.

 

© 2013-2014 Russian business network RussianPatents.com - Special Russian commercial information project for world wide. Foreign filing in English.