Patent Application
20090064805
The present invention provided is intended for keeping the direction given in the plane of inertial space. It can be used in the cases where use is required of a gyroscope, particularly, for solving the tasks of orientation, navigation, piloting (navigation), stabilization of different objects, etc.
For keeping the direction given in the plane of inertial space (further for short—the direction given) use is made of the method based on kinetic torque tending for keeping said direction in said plane to remain unchangeable.
For achieving the above, use is made of the device called a single-axis gyrostabilizer. It can be one-gyroscopic and two-gyroscopic [1].
The closest analog is considered to be two-gyroscopic single-axis gyrostabilizer, wherein the axes of inner gimbals of gyroscopes are connected by means of kinematical connection unit [1].
A stabilizing element tending for keeping said direction given in said one-axis gyrostabilizer is considered to be outer gimbals.
Any known one-axis gyrostabilizer is considered to have a considerable drawback consisting in the fact that under the influence of disturbance sign-constant harmful torques around the axis of any inner gimbals, said stabilizing element (outer gimbals) is said constantly “to go away” (to precession, damp, rotate) from said direction given towards one and the same side. This results in considerable continuous accumulation of the error in the course of time, which is considered to be unacceptable.
The object of the solution provided is increasing of the accuracy through using said stabilizing element, keeping said direction given in said plane of the inertial space, irrespective of the precessions of the gyroscopes, influence of harmful torques and turns in said plane of the movable object, whereon said direction is kept.
For accomplishing the object mentioned above the two one-axis gyrostabilizers are forced to have precessions towards the opposite sides. Herewith, the immovability of said stabilizing element of said connection unit connecting said gyrostabilizers in the plane of the inertial space is being kept.
For the purpose, around (relative to) said axes of said inner gimbals of said gyrostabilizers there are torques artificially created, by value they being knowingly greater than the maximum possible harmful torques acting around said axes.
Said torques according to the direction are so predetermined that said gyrostabilizers tend to precession towards the opposite sides.
The device to implement the method provided is called a gyro device
There are no scientific contradictory evidences for eliminating any harmful influence of certain changes of various (disturbance) harmful values and factors, according to the prior art.
Known logometers, for instance, are considered to eliminate any harmful influence of certain changes of the electric voltage to be supplied; in many devices any harmful influence of certain changes of external disturbances is eliminated, for instance, of temperature (by means of the temperature compensation schemes).
In addition, in said one-axis gyrostabilizer influence of any harmful (disturbance) torque is eliminated, the latter acting around said axis of its outer gimbals. Herewith, any opportunity of said error accumulation at the expense of said torque action is eliminated.
In the present solution provided any opportunity of said error accumulation not only at the expense of any harmful torques acting around said axis of said outer gimbals but also at the expense of any harmful torques acting around said axis of said inner gimbals is expected to be eliminated.
In the present solution provided use is made of the two gyrostabilizers being kinematically connected with each other forming an unified two-gyroscope system
Creation of tending to precessions of said gyrostabilizers towards the opposite sides or its precession towards the opposite sides is expected to eliminate “going away” in the plane given of the two-gyroscope system as a whole (in one and the same direction).
Each of said two one-axis one-gyroscope gyrostabilizers of said gyro device to be used is provided with the system of intergimbals (power) stabilization. Said system comprises an angle data transmitter (located along the axis of said inner gimbals) and the support mechanism (located along the axis of said outer gimbals).
It is base of said connection unit connecting the axes of said outer gimbals of said gyrostabilizers that is the stabilizing element. Said element is considered to remain unmovable in the plane given (of the inertial space) irrespective of the influence of disturbance (harmful) torques, precessions (or tending to them) of said gyrostabilizers and turns in said plane of the movable object, whereon use is made of said gyro device.
According to the solution there are provided two variants of the gyro devices.
In the 1st variant forced torques are created so that precessions of said gyrostabilizers towards the opposite sides occur with independent on each other, arbitrary, by value (module), angular velocities. In the variant mentioned above the immobility of said stabilizing element (in the plane of the inertial space) is performed by means of effects of self-brake (occurring on both sides of said stabilizing element). The device for implementing the 1st variant can be called-variation gyro device
In the 2nd variant forced torques are created so that possible precessions of said gyrostabilizers towards the opposite sides can occur only with such angular velocities, the ratio between them being strictly predetermined. In said variant said immobility of said stabilizing element (in said plane) is performed through constructive (kinematical) way. The device for implementing the 2nd variant is called logometric gyro device.
Said variation device comprises two one-axis gyrostabilizers connected with each other by said connection unit. Said unit comprises said stabilizing element, the role thereof being played by the carrier. On said carrier there is one or two electric motors of tracking and two dentate differential self-braking wheelworks (further for short—self-braking wheelworks) placed [2].
Each self-braking wheelwork is considered to have two central (sun) gears to be connected with each other by means of dentate pinions—satellites. One of said central gears is considered to be a spiral gear of self-braking worm-and worm pair, and another one—to be cylindrical gear, accordingly.
In case use is made of one said electric motor of tracking, then both its parts (an inductor and an armature) are put in bearings and connected with said cylindrical central gears. In case when use is made of two electric motors of tracking, then their bodies are tightly fastened on said stabilizing element (carrier), and their shafts (axles) are tightly connected with said central cylindrical gears.
The axes of said spiral gears are tightly connected, accordingly, with the axes of outer gimbals of said gyrostabilizers.
Said axes of said outer gimbals are located in said bearings of said body of said gyro device. Said body can be fastened on some kind of platform, by way of example, horizontal or directly on the body of the movable object, particularly, if said body is used as a horizontal platform [3].
Each self-braking wheelwork is used with positive gear-ratio not equal to 1. This means that with an unmovable carrier both central gears can rotate only in one and the same direction but at different angular velocities.
Herewith, said angular velocity of said cylindrical gear is expected to be less than the one of said spiral gear of said self-braking wheelwork.
Each one-axis gyrostabilizer is considered to have a system of intergimbals (power) stabilization comprising an angle-data transmitter (it being located along the axis of the inner gimbals) and, a support mechanism, (being located along the axis of the outer gimbals). Said support mechanism, receives a signal from said angle-data transmitter. Said support mechanism is considered to create, in the braking mode, the torque around the axis of said outer gimbals. Herewith, it is considered to hold the main axis of the gyroscope (the axis of its own rotation) in the position close to perpendicular relative to the axis of the outer gimbals of the gyroscope.
Around said axis of said outer gimbals of each gyrostabilizer the torque is forced to be created. Said torque is created with the help of the torque device located along the axis of the inner gimbals or (and) through disbalance. Such torques in gyroscopes are created of such direction that they precession towards the opposite directions.
The inner and outer parts of the electric motor of tracking (its inductor and armature) are considered to rotate central gears (towards the opposite directions), wherefrom said rotations through pinions are supplied to said spiral gears. From said spiral gears said torques are transmitted to said axes of said outer gimbals of said gyrostabilizers, where they are compensated by the systems of intergimbals stabilization (their support mechanisms).
From said electric motor of tracking said torques are not transmitted to said stabilizing element (carrier), due to self-braking. In addition, due to said self-braking the torques acting from outside on said stabilizing element are not considered to be able to cause its rotation either.
Thus, said stabilizing element is considered to remain unmovable all the time.
It should be kept in mind that since angular velocities of said spiral gears (they being equal to the velocities of said precessions of said gyrostabilizers) are considered to be rather small, then effects of self-braking in such cases are considered to remain unchanged.
In case of using the two electric motors of tracking, the rotor of each of them connected with said central cylindrical gear is considered to transmit rotation from it to the corresponding spiral gear.
As for the rest, the work with two electric motors of tracking is considered to be the same as with using one electric motor of that kind.
In the logometric gyro device two one-axis gyrostabilizers are located on said stabilizing element of said connection unit between them.
Said axes of outer gimbals 0 g said gyrostabilizers are connected with each other by means of gearing, comprising two gears tightly fixed on said axes.
Said of said outer gimbals of said gyrostabilizers are considered to be mutually parallel and parallel to the rotation axis of said stabilizing element, it being located in said bearings of the body of the gyro device.
The body of the gyro device can be fastened on some platform, by way example, horizontal, particularly, on the body of the movable object, if, in particular, said body is used as a horizontal platform [3].
Each gyrostabilizer is provided with the system of intergimbals (power) stabilization holding the main axis of the gyroscope (the axis of own rotation) in the position perpendicular to the axis of the outer gimbals. Said system comprises said angle data transmitter located along the axis of said outer gimbals of said gyroscope, and said support mechanism being located along the axis of the outer gimbals. of the gyroscope.
Said support mechanism comprises inner and outer parts (an inductor and armature). One of these parts is tightly fastened on the axis of the outer gimbals, and the two gears are tightly fastened with the axis of another gimbals. Said gears are connected by means of two gearings (with different gear-ratios) with the two gears tightly connected with said support mechanism of another gyrostabilizer.
Such double gearing with different gear ratios between support mechanisms is considered to eliminate any harmful influence of one system of intergimbals stabilization (power) on another one.
Let one of the gyrostabilizers be called driving and another—driven.
Along the axis of each inner gimbals said torque device is also located.
Said angle-data transmitter of the driving gyrostabilizer is electrically connected with said torque device of the driven gyrostabilizer.
Around said axis of said inner gimbals of said driving gyrostabilizer the torque is created being knowingly greater than the maximum possible oppositely acting harmful torque. Said torque can be created with the help of said torque device (whereon corresponding electric voltage is supplied) and (or) through disbalance.
From said angle-data transmitter of said driving gyrostabilizer a signal to said torque device of said driven gyrostabilizer is transmitted.
Thus, in said logometric gyrostabilizer there are gearings between the axes of the outer gimbals of the gyrostabilizers and between the support mechanisms. Due to such gearings with known gear-ratios there is one of the two opportunities: either gyroscopes don't precession (their angular velocities of precessions being equal to zero) or they do precession towards the opposite directions with previously known ratios of angular velocities, particularly, equal to “−1”. With any of such opportunities said stabilizing element is considered to remain unmovable.
The present technical solution is illustrated, by way of example, in the accompanying drawings, in which:
FIG. 1—a scheme of one-motor variation gyro device;
Fig.—a scheme of the connection of the two electric motors of tracking with central cylindrical gears;
Fig.—a scheme of logometric gyro device.
According to the present technical solution the method of keeping the direction given on the movable object consists in giving tending to precessions (or precessions) towards the opposite sides for one-axis gyrostabilizers to be mechanically connected with each other by the connection unit.
Said connection unit comprises said stabilizing element remaining unmovable in the plane of the inertial space irrespective of acting of any harmful torques, precessions (or tending to them) of gyrostabilizers and turns of the movable object in said plane.
The device implementing the method provided is called a gyro device.
Two types of said gyro devices are considered to be possible: variation and logometric.
In said variation gyro device angular velocities of the precessions of both gyrostabilizers can be arbitrary, i.e. between them there is no ratio.
In said gyro device immovability of said stabilizing element is kept by means of the two effects of self-braking, the latter occurring on either side of said element.
The schemes of said variation device are shown in
In said logometric gyro device between possible angular velocities of said precessions there is strict previously known ratio, though the values of said velocities are unknown.
In said logometric gyro device immovability of said stabilizing element is kept by means of kinematically constructive way.
Said variation gyro device can be one-motor (
Said variation gyro device comprises two one-axis gyrostabilizers 11 and 12, said connection unit 21, said electric motor of tracking 3 (
Said base 5 of said connection unit is considered to be said stabilizing element.
On said element there are two self-braking differential wheelworks located (further—self-braking wheelworks) 61 and 62 [2]. Thus, said stabilizing element is considered to the carrier for said wheelworks.
Said self-breaking wheelwork 61 comprises said cylindrical gears 71, 81, 91; conical gears 101 and 111 and said self-braking worm-and worm pair 121, it comprising a worm 131 and said spiral gear 141. In said self-braking wheelwork 61 an input axis is the axis of rotation of said gear 71, and an output one—the axis 151 of rotating said spiral gear 141.
Said self-breaking wheelwork 62 comprises said cylindrical gears 72, 82, 92; conical gears 101 and 111 and said self-braking worm-and worm pair 122, it comprising a worm 132 and said spiral gear 142. In said self-braking wheelwork 62 an input axis is the axis of rotation of said gear 72, and an output one—the axis 152 of rotation of said spiral gear 142.
Said gears 71 and 72 as well as 141 and 142 are considered to be central (sun) gears of said self-braking wheelworks 61 and 62.
Said axes 151 and 152 of said outer gimbals 161 and 162 of said gyrostabilizers 11 and 12 are considered to be tightly connected with said axes of spiral gears 141 and 142, correspondingly, i.e. with the output axes of said wheelworks 61 and 62.
Said electric motor of tracking 3 comprises said inner part (rotor) 17 and outer part (body) 18. Both these parts in the process of operation are considered to be movable (rotating). The axis of said rotor 17 is tightly connected with said input axis of said wheelwork 61, and the axis of said body 18 is tightly connected with said outer axis of said wheelwork 62.
Said gyrostabilizer 11 is considered to have said system of said intergimbals (power) stabilization comprising said angle-data transmitter 191, and said support mechanism 201.
Said gyrostabilizer 12 is considered to have said system of said intergimbals (power) stabilization comprising said angle-data transmitter 192, and said support mechanism 202.
As said angle-data transmitter use can be made of an inductive sensor, a selsyn, a potentiometer and others.
Said systems of said intergimbals (power) stabilization are considered to hold the main axes of said gyroscopes being approximately perpendicular to the axes of said outer gimbals. In
Said torques created by said electric motors of tracking and harmful torques (friction, disbalance, and others) are considered to be compensated by the torques created by said support mechanisms.
On said 221 and 222 of said inner gimbals 231 and 232 there are torque devices 241 and 242 located.
It is desirable (but not obligatory) that the weight of said connection unit should cause similar pressures on both gyrostabilizers, for the purpose, provision can be made of limit stops 251 and 252 being tightly fastened on the axes of said outer gimbals of said gyrostabilizers.
Said outer gimbals of said gyrostabilizers can be fastened by means of one of known methods (by means of the stabilizing platform or by means of gyro vertical or analogously to that as it is done in gyro units of course systems and others), perpendicular to the plane given, wherein there is initial (given) direction (on the drawing it is not shown not to make them more complex) kept.
Let's consider positive direction of angular velocity (and moment of forces) of some element to be the direction, wherein said one-axis gyrostabilizer 11 precessions (around said axis of said outer gimbals). This direction, for example, is counter-clockwise, if said gyrostabilizer is looked from above. Then the direction of precession of said one-axis gyrostabilizer 12 around its axis of said outer gimbals is expected to be negative.
In the process of on-switching by means of caging devices (they are not shown on the drawings attached) and systems of intergimbals (power) stabilization the main axes of said gyrostabilizers are fastened perpendicular to said axes of said outer gimbals. In the process of further work said systems of intergimbals stabilization are expected to hold the main axes of said gyrostabilizers in above position.
Angular velocities of precessions of said gyrostabilizers (ω1 and ω2) are considered to be created by the torques M1 and M2 correspondingly applied relative to (around) said axes of said inner gimbals of said gyrostabilizers by said torque devices 191 and 192. The values and signs of said torques M1 and M2 are to be such that precessions of said gyrostabilizers (around said axes of said outer gimbals) occur towards the opposite sides. For example, they being as such that said gyrostabilizer 11 precessions at angular velocity ω1 in the positive direction, and said gyrostabilizer 12—at angular velocity ω2, accordingly, in the negative direction, irrespective of any possible changes of the parameters of said gyro device and environmental conditions.
For providing opportunities of the precessions mentioned said electric motor of tracking 3 is considered to be used. In the process of operation on said motor there is such electric voltage supplied that its maximum possible angular velocity (brought to said axes of said outer gimbals) were a bit greater than the amount of the maximum possible angular velocities of said precessions of said gyrostabilizers (the same with said spiral gears tightly fastened with said axes of said outer gimbals).
Said inductor and armature (17 and 18) of said electric motor 3, they rotating in the opposite directions, through the system of gears are considered to make uninterrupted pressing of worm cogs (131 and 132) to the cogs of spiral gears (141 and 142).
Due to self-braking of driving torque from said electric motor of tracking 3 to said stabilizing element (carrier) 5 are not expected to be supplied {2}. Harmful torque applied to said stabilizing element is not expected to be able to cause its rotation because of two reasons: a) the torque of pressing said cogs is chosen so that, by value, said harmful torque were not able to surmount it; b) because of self-braking.
Taking the above into amount, as well as the fact that said connection unit is connected with said gyroscopes, the former as well as said gyroscopes are not expected to take part in the rotations of the movable object (in said plane of the direction given, i.e. around said axes of said outer gimbals).
The torque applied to said stabilizing element without creating the rotation is considered to cause its angular shifting, at least, within flexibility (part of an arc second), irrespective of any changes of angular velocities of said precessions
Thus, said stabilizing element remains unmovable in said plane of the inertial space, irrespective of acting disturbance factors (in particular, any harmful elements), precessions of stabilizers and turns in said plane of the movable object.
Immovability of said stabilizing element can be implemented by means of the two electric motors of tracking—in the two-motor gyro device (
In said gyro device on said stabilizing element (carrier) 52 there are two said electric motors of tracking 41 and 42 fastened. Herewith, said outgoing axle (shaft) is tightly connected with the axis of said gear 71, said outgoing axle (shaft) of said electric motor of tracking 42 is tightly connected with said axis of said gear 72.
It is desirable to use built-in reduction units inside the bodies of said electric motors (in this case it is possible to use high speed electric motors and small-size ones as well).
With using said two-motor gyro device it is not required that any constructive changes in said electric motor of tracking be made (in one-motor gyro device it is necessary not only to position said rotor of said electric motor but also its body on the bearings).
On said electric motors of tracking there are such electrical voltages supplied that the maximum possible angular velocity of each of them (brought to corresponding axis of said outer gimbals) were a bit greater than the maximum possible compared to the angular velocity of precessions of the corresponding gyrostabilizer (so that said torque of pressing said cogs were greater than the maximum possible harmful torque).
It is desirable that similar electric motors 41 and 42 be used for the difference torque on the part of the bodies whereof to be close to zero.
As for the rest, the operation of said two-motor gyro device is the same as tat of said one-motor gyro device.
The possibility of implementing the solution provided (its workability) is proved by the following:
The authors are quite sure that there is nothing that can be at variance with the above.
Said logometric gyro device comprises (
Parallel axes 153 and 154 of said outer gimbals 163 and 164 of said gyrostabilizers 13 and 14 are located in said bearings of said stabilizing element 53.
Said stabilizing element 53 is considered to have the axis of rotation 35, it being located in the bearings of some platform (for example, horizontal or vertical) or in the bearings of the object, whereon there is said logometric gyro device located.
Said gears 27 and 28 being the integral part of hooking are considered to be tightly fastened on said axes 153 and 154 of said outer gimbals 163 and 164 of said gyrostabilizers 13 and 14.
In
Said axes 223 and 224 of said outer gimbals 233 and 234 are located in said bearings of said outer gimbals, and the main axes are located in said bearings of said inner gimbals.
Said system of intergimbals (power) stabilization of said gyrostabilizer 13 comprises said angle-data transmitter 193 and said support mechanism 361. One of the parts (371) of said support mechanism is fastened on the axis 153 of the outer gimbals 163, and another part (381) is located in the bearings of said stabilizing element 53.
The output of said angle-data transmitter 193 is connected electrically with the input of said support mechanism 361.
Said system of intergimbals (power) stabilization of said gyrostabilizer 14 comprises said angle-data transmitter 194 and support mechanism 362. One of the parts (372) of said support mechanism is fastened on the axis 154 of the outer gimbals 164, and another part (382) is located in the bearings of said stabilizing element 53.
The output of said angle-data transmitter 194 is connected electrically with the input of said support mechanism 362.
The axes of said gears 30 and 31 are located in the bearings of said stabilizing element 53.
The axes of said gears 321. and 322. are tightly fastened with corresponding axes of said support mechanisms.
Said gears 30, 331. and 332 are considered to be spurious. Said gears 331. and 332 as well as said gear 30 are located in the bearings of said stabilizing element.
The axes of said gears 341. and 342 are tightly fastened with the axes of the axes of said gears 321. and 322.
Gear ratio from said gear 321 to said gear 322 has been chosen unlike gear ratio from said gear 341 to said gear 342. Owing to that the torques from one support mechanism to another support mechanism and to said stabilizing element are not transmitted (they are damped by said torques of gears torsion). And since said gear ratios are considered to be close by value then said torques of torsion turn out to be insignificant. Thus, intergimbals (power) systems of stabilizations are considered to work independently one on another.
Since gear-ratio of said connection unit 26 (its gears 27 and 28) is considered to be negative, then there are two cases possible: either both gyroscopes of gyrostabilizers are considered to be unmovable, or they precession towards the opposite sides (around the axes of outer gimbals).
For said gyro device not to precession as a whole (around the axis 35 of said stabilizing element) forced torques are applied around (relative to) said axes of said inner gimbals of said gyrostabilizers in the way that they knowingly were greater the maximum possible harmful torques around (relative to) said axes and tend to cause precessions of said gyrostabilizers towards the opposite sides.
Creation of said torques is considered to be possible by means of disbalance of said gyrostabilizers (around said axes of their inner gimbals) and by means of said torque devices.
In
Said angle-data transmitter 193 of said gyrostabilizer 13 is considered to be electrically connected with said torque device 244.
Since said precession of said logometric device as a whole around said axis 35 is considered to be impossible, and said stabilizing element is kinematically connected with said gyroscopes, then said element is considered to remain unmovable in the plane of inertial space (perpendicular to said axes of said outer gimbals, and irrespective of the action of any disturbance factors, precessions (or tending to them) of said gyrostabilizers and the rotation in that plane of the movable object, whereon said gyro device is located.
Let's consider the operation of the logometric gyro device provided by means the drawing
Let said axes of said outer gimbals of gyrostabilizers 13 and 14 as well as said axis 35 of said stabilizing element (both being parallel to each other) by means of some known way be located perpendicular to the plane given of inertial space, wherein it is necessary to keep immovability of said stabilizing element.
It is known that usually said gyroscope device is provided with said caging device. Since such device is known and its image would make understanding of the plot of the solution provided more complicated, then in
Said caging device is considered to operate only at initial moment supplying power, and is designed for quick bringing said gyroscope device to the initial position, thereafter said caging device is off.
In said logometric gyro device the initial position is considered to be perpendicularity of said axes of said outer gimbals of said gyrostabilizers, and thus, said axis 35 of said stabilizing element of the plane give and the perpendicularity of the main axes of said gyroscopes to said axes of their outer gimbals.
Let said gyrostabilizer 13 be considered driving and said gyrostabilizer 14—driven accordingly.
When switching on after caging (or in the process of caging) the voltage given u1 is supplied to said torque device 243 of such value that occurring torque (of forces) M1 relative to (around) said axis 223 were greater than the maximum possible one of harmful torque Mr1 relative to (around) the same axis and of such sign that there occurred tending to precession of said gyrostabilizer 13 in the direction given, for example, in the positive direction (as shown by an arrow in
Since said gyrostabilizers 13 and 14 are considered to be kinematically connected with each other by said gearing 26, then due to the main property of said gyroscope said gyrostabilizer 14 prevents such tending. But since M1>Mr1, then the main axis 213 of said gyrostabilizer 13 is expected to rotate around said axis 223 in the direction of acting said torque M1. Herewith, the rotor of said angle-data transmitter 193 rotates by the angle β1. From output of said angle-data transmitter 193 signals u2 are expected to be supplied to said torque device 244, and support mechanism 361. Said signal u2 is considered to create said torque M2 relative to (around) said axis 224 of such direction that there will occur tending of said gyrostabilizer 14 to precession in the negative direction. Simultaneously, said signal u2 is considered to create said torque of said support mechanism, the latter tending to decrease said angle β1. Under the action of said torque M2 the main axis 214 is expected to rotate by the angle β2, in consequence of the above, said support mechanism 362 is expected to tend to decrease said angle (β2). When said torque M2 is greater than torque of resistance Mr2 acting relative to (around) said axis 224 there will occur tending of said gyrostabilizer 14 to precession in the negative direction. And, finally, as increasing said torque M2, there will occur the situation, whereby said torque M2 is expected to create said angular velocity of precession ω2 to be equal to said angular velocity ω1. The values (modules) of said angular velocities ω1 and ω2 are expected to increase till the time there occurs the torques balance.
It should be kept in mind that said gyrostabilizers are not only acted by said torques created by said torque devices, said support mechanisms, said harmful torques of resistance and gyroscopic torques there might occur also the torque of gyrostabilizers interaction, it being caused by pressing gears cogs 27 and 28.
Said torque (of pressing) is considered to be regulating, tending to provide equation ω1=ω2. For example, if there is tending to extreme increase of said velocity ω1, then gear cogs 27 are considered to be pressed to said gear cogs 28, which is expected to result in increasing said angle β1. Thus, consequently, u2, M2, ω2 will be increased and again, balance will occur when ω1=ω2. Or, for example, if there tending to extreme increase of velocity ω2 then, gear cogs 28 are expected to be pressed to gears cogs 27, which will, eventually, result in getting rid of said tending.
Thus, considering the operation of said logometric gyro device leads to the following conclusions:
Thus, said stabilizing element in any of said gyro devices provided is considered to remain unmovable in the plane of inertial space, irrespective of the action in said plane of any harmful torques, precessions (or tending to them) of gyrostabilizers and turns in said plane of the movable object.
Using the solution provided will allow it to eliminate accumulation of the error in the course of time, and, hereby, to considerably increase the accuracy of different devices, wherein use is made of gyroscopes.
Since in the solution provided use can be made of the gyroscope of low accuracy, then said gyro device (both variation and logometric) can be implemented in small-size version.
The solutions of the problems of keeping the direction given and determining the vertical [3] with superior accuracy allow it to meet the problems of independent determination of the location, eliminating the accumulation of the error in the course of time. This solution based on the latest equations of navigation obtained by the authors will be submitted for patenting.
| Number | Date | Country | Kind |
|---|---|---|---|
| 185846 | Sep 2007 | IL | national |
