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The Most Sensitive Part Of A Combat Aircraft!!!

Levina

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girka2ijae6givozeqld.jpg



It look like something Doc Brown would be working on in his garage, but it is absolutely one of the most essential and sensitive technologies found on many military and some civilian aircraft today: The Ring Laser Gyroscope.

Introduced in the mid 1960s and developed rapidly from then on, the Ring Laser Gyroscope has taken the place of many larger and more complex mechanical gyroscope systems. In comparison to their predecessors, Ring Laser Gyros can be built much smaller, they do not resist changes in direction, are totally frictionless, have low power consumption, and feature almost no moving parts, thus they are incredibly reliable, while still providing adequate accuracy.

erede6p0aqewuia0ngvg.jpg


Ring Laser Gyroscope's small size has also made them particularly well suited for tactical aircraft, both manned and unmanned, and weapon systems that once had to rely on much bulkier inertial navigation systems made up of accelerometer and mechanical gyroscopes. These include bombers, surface combatants, satellites and submarines. Additionally, this technology has migrated to the commercial marketplace, and many modern airliners and ships also feature RLG technology in their navigational suites.

Today, modern inertial navigational suites found on some aircraft, submarines, ships and spacecraft use Ring Laser Gyroscopes as part of an integrated Inertial Navigation Systems (INS), and in some cases, fly-by-wire flight control systems and targeting pods use them as well.

Inertial navigation systems with integrated GPS can pair gyroscopes, and in many cases Ring Laser Gyroscopes, and accelerometers with a GPS receiver system. Software within the system cross-checks the readings of each discreet navigational sensor source, and possibly other sources such as radio navigational beacons, flight data such as airspeed and attitude, and doppler and radar altimeter data to come up with an 'agreed upon' position.

Generally speaking, if one of the sensors of data sources used by the INS begins to deviate from the majority of the sources, or from a more heavily weighted source as computed in the software's 'voting' algorithms, then less weight will be given to the deviating source. If a source is way off position in comparison to others, or showing signs of failure, it could be filtered out by the INS software entirely. This leaves a less precise positioning capability, but not one that is entirely compromised due to a single failed or spoofed discreet sensor within the system. Sometimes multiple Ring Laser Gyroscopes will be used in a single Inertial Navigation System to work in tandem for redundancy reasons or for automatic cross-checking.

fm0suo035nwsuis8gnlc.jpg


Gyroscopes can also be used to help stabilize an aircraft in flight and for autopilot purposes. According to Honeywell, one of the world's leaders in Ring Laser Gyroscope systems, the technology dates back a century: (correction: its not ring laser gyroscopes that date back a century but the gyroscope techonology)

Developed by inventive genius Elmer Sperry, the device was first demonstrated by Sperry's son Lawrence during France's Airplane Safety Contest in June 1914.

During the demonstration flight over the Seine River, Lawrence let go of the controls, stood up in the cockpit and raised his hands high above his head. Then came a roar of approval from the crowd gathered below as his mechanic walked far out onto the wing and the plane remained level.

As the Sperrys' flight demonstrated, a gyroscopic autopilot could fly an aircraft straight and level on a compass course without a pilot's constant attention. As a result, pilots could fly further without becoming fatigued, improving safety and setting the stage for the longer-distance flights that would would become popular with the rise of commercial aviation in the decades to come.

Today, this technology has moved beyond just autopilots, as Ring Laser Gyros can also be used for stabilizing an aircraft in space when its data is tied to an aircraft's fly-by-wire flight control system. For instance, the 'carefree handling' capabilities found on modern fighter aircraft allows aircrews to literally point the jet where they want it to go with minimal coordinated control or thought given to the aircraft's gross weight and configuration. The F-35B's hovering capability is possibly one of the most exotic examples of this.

nfxroufnyr9gxfxe33ig.jpg


Unlike the Harrier, where a pilot has to baby the aircraft in hover mode as if it were teetering on top of a telephone pole, the F-35B has a highly simplified fly-by-wire control system, one that even allows a pilot to take their hands off the controls, resulting in the aircraft steadily holding its position in midair.



Ring Laser Gyros' lack of moving parts and small size, such as the Honeywell HG1900 IMU which weighs under two pounds, and the HG1700 IMU which weighs under a pound, make them ideal for integration on guided munitions. The Joint Direct Attack Munition (JDAM),Paveway IV dual mode laser guided bomb, use these units, along with GPS, to execute incredibly pinpoint attacks on their targets. Also, the inclusion of a competent INS system along with GPS means that if a GPS signal is jammed or lost, the munition still has a high-probability of effecting its intended target.

jzcyogthcvo4f105ziwr.jpg


Virtually all advanced smart munitions have a integrated INS systems featuring Ring Laser Gyros, from Tomahawks and advanced air-to-air missiles, to guided artillery shells. Yes, artillery shells. These howitzer rounds present their own unique problems to something as miniaturized and sensitive as Ring Laser Gyroscope.

A 155mm artillary shell will experience well over 10,000 times the force of gravity as it is fired, and seeing as payload (ie explosives) needs to be maximized on these rounds, stuffing a hardened guidance system into a 100lb artillery shell is challenge to say the least. Micro Electro-Mechanical Systems (MEMS) technology has allowed such a feat to become a reality, and Honeywell's HG1930 Gun Hard IMU can withstand up to 20,000 times the force of gravity and still be ready to guided the round on its way to its intended target. This is truly amazing technology that is being tested today on the Army's M982 Excalibur 155mm guided round.

mnribm48kusoqiu93vkj.jpg



The Navy is taking the guided artillery round one step further with its 155mm Long Range Land Attack Projectile (LRLAP). This will be the primary precision weapon for the DDG-1000 Zumwalt Class' advanced deck gun system. This rocket assisted artillery round will fly out to over 75 miles to impact its target within about 100 feet or less. Like the Excalibur artillery round, the Navy's LRLAP will use a GPS embedded INS, including a hardened and miniaturized Ring Laser Gyroscope, to navigate its way to its final destination.

As Ring Laser Gyroscopes and integrates INS technology continues to shrink, smaller and smaller unmanned aircraft, and the micro-munitions they carry, will be capable of incredibly precise navigation, even in areas where GPS is denied.

GPS not being a guaranteed resource during a time of war is a real possibility in potential future peer-state conflicts, where space could be a battleground in itself. Advanced jamming and GPS spoofing technologies that are already being fielded today also pose a major threat to GPS dependent systems. This means that in a battle against a capable foe, the non-GPS dependent components in modern Inertial Navigation Systems, Ring Laser Gyros included, may be relied upon more than ever before in mankind's post-GPS navigational history.

ps16ishc7b4eberugstz.jpg


(Photo clicked during exercise valiant shield, largest exercise carried out after Vietnam war and it was the first time observers from China were allowed Exercise Valiant Shield - Wikipedia, the free encyclopedia )



@Abingdonboy
I just stumbled upon this article on another site and was completely awed by what I read about this tiny device. Now I've 2 doubts 1) if ring laser gyroscopes 're commonly used then why do only F-35Bs have hoovering capabilities??
2) I have not seen many pics where bombers lead the pack, is it common???
 
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Research Centre Imarat (RCI)'s Ring laser Gyro with a square laser cavity of cavity length 28 cms. This system is intended for use aboard the LCA and missiles with longer flight time.

in_rlg_001.jpg
 
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Research Centre Imarat (RCI)'s Ring laser Gyro with a square laser cavity of cavity length 28 cms. This system is intended for use aboard the LCA and missiles with longer flight time.

in_rlg_001.jpg

I searched and realised that the Sagem SIGMA 95N ring-laser gyroscopes in LCA 're french, and not made in India.
 
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Submarines, tanks, torpedoes & UAVs get Indian nav systems



Outsmarting the know-how denials imposed by the West under the Missile Technology Control Regime (MTCR), Inertial Navigation Systems (INS) developed in India are steadily finding a confirmed seat onboard multiple military platforms. The Research Centre Imarat (RCI) in Hyderabad today seems to have graduated in all the major technology areas of navigation, including sensors, SATNAV (satellite navigation) receivers, navigational aids, algorithms\schemes for different applications and infrastructure development. In the process, India has elevated its status on par with a handful of nations possessing a wide spectrum of sensor technologies.


The dynamically-tuned mechanical gyroscopes (DTG), optical–ring laser and fiber-optic gyroscopes, micro-gyroscopes and high-accuracy force balanced accelerometers (which measures the acceleration) are some hitherto-alien technologies now in India's command. (Gyroscopes are instruments that senses rotation). "Mastering these sensor technologies made the total independence from Western nations. These advancements have offered greater flexibility to configure and customize varied classes of INS of the users' choice," RCI sources said. "All missions are of very high precision strike capabilities, which is primarily decided by the accuracy of the INS. Today, we are on par with world leaders offering RLG-based (ring laser gyro) INS," sources said.


Agni-IV is the first missile on which a design version of RLG-based INS was used in mission mode successfully, probably signaling an end to imports in this segment. The navigation aids based on the different classes of inertial sensors developed by RCI is said to be not only meeting the requirements of strategic and tactical missile programmes, but are being heavily employed on combat aircraft, ships, submarines, tanks, unmanned aerial vehicles, torpedoes and smart munitions.


“The development ranges from highly miniaturized micro sensors-based system weighing around 300g for smart bombs and PGMs (precision-guided munitions) to a very-high accuracy 30 kg system for long-endurance naval applications,” sources said. Ultra high accuracy sensors development is already initiated for future needs of space and very long range missions.


The Inertial System Group at RCI is silently delivering solutions enhancing the multi-platform launch capability of the flight vehicle from ships (Rajput Class), submarines and aircraft (LCA & Sukhoi). “Our capabilities in the navigation systems are now being explored by world leaders who are keen to join hands for collaboration. The roles have been reversed and we are in pursuit of developing Navigation On Chip (a dream of A P J Abdul Kalam), which aims at miniaturization of systems, making them reliable and cost-effective,” sources said.


The preliminary development of a single chip NGC (Navigation, Guidance and Control) has already taken birth with System on Chip (SOC), SATNAV on Chip close to realisation. This will enable a low cost, low volume, low power and highly reliable system available for majority of the tactical and micro-air vehicles. "The energy requirements of the vehicle(s) will drop drastically and India will become a world leader in the critical area of navigation," sources said
 
.
girka2ijae6givozeqld.jpg



It look like something Doc Brown would be working on in his garage, but it is absolutely one of the most essential and sensitive technologies found on many military and some civilian aircraft today: The Ring Laser Gyroscope.

Introduced in the mid 1960s and developed rapidly from then on, the Ring Laser Gyroscope has taken the place of many larger and more complex mechanical gyroscope systems. In comparison to their predecessors, Ring Laser Gyros can be built much smaller, they do not resist changes in direction, are totally frictionless, have low power consumption, and feature almost no moving parts, thus they are incredibly reliable, while still providing adequate accuracy.

erede6p0aqewuia0ngvg.jpg


Ring Laser Gyroscope's small size has also made them particularly well suited for tactical aircraft, both manned and unmanned, and weapon systems that once had to rely on much bulkier inertial navigation systems made up of accelerometer and mechanical gyroscopes. These include bombers, surface combatants, satellites and submarines. Additionally, this technology has migrated to the commercial marketplace, and many modern airliners and ships also feature RLG technology in their navigational suites.

Today, modern inertial navigational suites found on some aircraft, submarines, ships and spacecraft use Ring Laser Gyroscopes as part of an integrated Inertial Navigation Systems (INS), and in some cases, fly-by-wire flight control systems and targeting pods use them as well.

Inertial navigation systems with integrated GPS can pair gyroscopes, and in many cases Ring Laser Gyroscopes, and accelerometers with a GPS receiver system. Software within the system cross-checks the readings of each discreet navigational sensor source, and possibly other sources such as radio navigational beacons, flight data such as airspeed and attitude, and doppler and radar altimeter data to come up with an 'agreed upon' position.

Generally speaking, if one of the sensors of data sources used by the INS begins to deviate from the majority of the sources, or from a more heavily weighted source as computed in the software's 'voting' algorithms, then less weight will be given to the deviating source. If a source is way off position in comparison to others, or showing signs of failure, it could be filtered out by the INS software entirely. This leaves a less precise positioning capability, but not one that is entirely compromised due to a single failed or spoofed discreet sensor within the system. Sometimes multiple Ring Laser Gyroscopes will be used in a single Inertial Navigation System to work in tandem for redundancy reasons or for automatic cross-checking.

fm0suo035nwsuis8gnlc.jpg


Gyroscopes can also be used to help stabilize an aircraft in flight and for autopilot purposes. According to Honeywell, one of the world's leaders in Ring Laser Gyroscope systems, the technology dates back a century: (correction: its not ring laser gyroscopes that date back a century but the gyroscope techonology)

Developed by inventive genius Elmer Sperry, the device was first demonstrated by Sperry's son Lawrence during France's Airplane Safety Contest in June 1914.

During the demonstration flight over the Seine River, Lawrence let go of the controls, stood up in the cockpit and raised his hands high above his head. Then came a roar of approval from the crowd gathered below as his mechanic walked far out onto the wing and the plane remained level.

As the Sperrys' flight demonstrated, a gyroscopic autopilot could fly an aircraft straight and level on a compass course without a pilot's constant attention. As a result, pilots could fly further without becoming fatigued, improving safety and setting the stage for the longer-distance flights that would would become popular with the rise of commercial aviation in the decades to come.

Today, this technology has moved beyond just autopilots, as Ring Laser Gyros can also be used for stabilizing an aircraft in space when its data is tied to an aircraft's fly-by-wire flight control system. For instance, the 'carefree handling' capabilities found on modern fighter aircraft allows aircrews to literally point the jet where they want it to go with minimal coordinated control or thought given to the aircraft's gross weight and configuration. The F-35B's hovering capability is possibly one of the most exotic examples of this.

nfxroufnyr9gxfxe33ig.jpg


Unlike the Harrier, where a pilot has to baby the aircraft in hover mode as if it were teetering on top of a telephone pole, the F-35B has a highly simplified fly-by-wire control system, one that even allows a pilot to take their hands off the controls, resulting in the aircraft steadily holding its position in midair.



Ring Laser Gyros' lack of moving parts and small size, such as the Honeywell HG1900 IMU which weighs under two pounds, and the HG1700 IMU which weighs under a pound, make them ideal for integration on guided munitions. The Joint Direct Attack Munition (JDAM),Paveway IV dual mode laser guided bomb, use these units, along with GPS, to execute incredibly pinpoint attacks on their targets. Also, the inclusion of a competent INS system along with GPS means that if a GPS signal is jammed or lost, the munition still has a high-probability of effecting its intended target.

jzcyogthcvo4f105ziwr.jpg


Virtually all advanced smart munitions have a integrated INS systems featuring Ring Laser Gyros, from Tomahawks and advanced air-to-air missiles, to guided artillery shells. Yes, artillery shells. These howitzer rounds present their own unique problems to something as miniaturized and sensitive as Ring Laser Gyroscope.

A 155mm artillary shell will experience well over 10,000 times the force of gravity as it is fired, and seeing as payload (ie explosives) needs to be maximized on these rounds, stuffing a hardened guidance system into a 100lb artillery shell is challenge to say the least. Micro Electro-Mechanical Systems (MEMS) technology has allowed such a feat to become a reality, and Honeywell's HG1930 Gun Hard IMU can withstand up to 20,000 times the force of gravity and still be ready to guided the round on its way to its intended target. This is truly amazing technology that is being tested today on the Army's M982 Excalibur 155mm guided round.

mnribm48kusoqiu93vkj.jpg



The Navy is taking the guided artillery round one step further with its 155mm Long Range Land Attack Projectile (LRLAP). This will be the primary precision weapon for the DDG-1000 Zumwalt Class' advanced deck gun system. This rocket assisted artillery round will fly out to over 75 miles to impact its target within about 100 feet or less. Like the Excalibur artillery round, the Navy's LRLAP will use a GPS embedded INS, including a hardened and miniaturized Ring Laser Gyroscope, to navigate its way to its final destination.

As Ring Laser Gyroscopes and integrates INS technology continues to shrink, smaller and smaller unmanned aircraft, and the micro-munitions they carry, will be capable of incredibly precise navigation, even in areas where GPS is denied.

GPS not being a guaranteed resource during a time of war is a real possibility in potential future peer-state conflicts, where space could be a battleground in itself. Advanced jamming and GPS spoofing technologies that are already being fielded today also pose a major threat to GPS dependent systems. This means that in a battle against a capable foe, the non-GPS dependent components in modern Inertial Navigation Systems, Ring Laser Gyros included, may be relied upon more than ever before in mankind's post-GPS navigational history.

ps16ishc7b4eberugstz.jpg


(Photo clicked during exercise valiant shield, largest exercise carried out after Vietnam war and it was the first time observers from China were allowed Exercise Valiant Shield - Wikipedia, the free encyclopedia )



@Abingdonboy
I just stumbled upon this article on another site and was completely awed by what I read about this tiny device. Now I've 2 doubts 1) if ring laser gyroscopes 're commonly used then why do only F-35Bs have hoovering capabilities??
2) I have not seen many pics where bombers lead the pack, is it common???

The Irony is this is nothing more than riding a bicycle, after all it is based on the principle of balancing the bicycle.
 
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The Irony is this is nothing more than riding a bicycle, after all it is based on the principle of balancing the bicycle.
Right!
The angulur momentum of the turning bicycle wheels makes them act like gyroscopes to help stabilize the bicycle. This gyroscopic action also helps to turn the bicycle.
But I would say Ring Laser Gyroscope uses Doppler principle to measure differences in laser light beams. :)
 
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@Abingdonboy
I just stumbled upon this article on another site and was completely awed by what I read about this tiny device. Now I've 2 doubts 1) if ring laser gyroscopes 're commonly used then why do only F-35Bs have hoovering capabilities??
Ma'am, it is not for the lack of a Ring Laser Gyroscope that more a/c don't have hovering capabilities but that requirement (V/STOL) is very niche and also very difficult to design and many would argue very flawed (the Harrier was notoriously dangerous to fly, subsonic and had poor range and the insistence on a V/STOL F-35 variant has seriously hampered that project's development). On the F-35 the lift fan and downward swooping engine where very hard to develop.
 
.
Right!
The angulur momentum of the turning bicycle wheels makes them act like gyroscopes to help stabilize the bicycle. This gyroscopic action also helps to turn the bicycle.
But I would say Ring Laser Gyroscope uses Doppler principle to measure differences in laser light beams. :)

How are they going to balance the light beams because a normal gyroscope is kept in a solution so that it can work in 3 dimensions? Moreover can the light beams be controlled i.e increase or decrease the number of light beam frequency because doppler frequencies can be reduced or increased to find the target range and size.
 
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How are they going to balance the light beams because a normal gyroscope is kept in a solution so that it can work in 3 dimensions?
I thought Ring laser gyroscopes exploits sagnac effect to its advantage and I dont see any solution in ring laser gyroscopes

1.jpg


ACE OF THE AIR said:
Moreover can the light beams be controlled i.e increase or decrease the number of light beam frequency because doppler frequencies can be reduced or increased to find the target range and size.
well rather than detecting time of travel differences of the laser beam split into 2 beams inside the RLG, the detectors measure differences in frequency, using the Doppler principle which is the basis of range-finding radars. The beam that is traveling in the direction of rotation of the platform has a longer distance to travel and thus a lower frequency while the beam traveling against the direction of motion has a shorter path and a higher frequency. The difference in frequency is directly proportional to the rotation rate.
 
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As the Sperrys' flight demonstrated, a gyroscopic autopilot could fly an aircraft straight and level on a compass course without a pilot's constant attention. As a result, pilots could fly further without becoming fatigued, improving safety and setting the stage for the longer-distance flights that would would become popular with the rise of commercial aviation in the decades to come.

Today, this technology has moved beyond just autopilots, as Ring Laser Gyros can also be used for stabilizing an aircraft in space when its data is tied to an aircraft's fly-by-wire flight control system.

According to this your
The beam that is traveling in the direction of rotation of the platform has a longer distance to travel and thus a lower frequency while the beam traveling against the direction of motion has a shorter path and a higher frequency. The difference in frequency is directly proportional to the rotation rate.

would indicate that it is going to work at a constant speed at all times. Hence this is only going to work on 1 dimension (the horizontal plain.) Wings Levelled flight characteristics.

This is just going to be providing vertical lift capability, However it would be interesting to note that there is no mention on how to compensate in case of any other force i.e engine failure, strong winds, unstable pitch due to many atmospheric conditions.

One must also not undermine that lift is produce by relative wind speed that allows an aircraft to glide, just before landing there is ground effect which is normally calculated to be at almost half the wing length. In VTOL this does not exist.
 
. . . . .
Looks like these ones are gonna replace them
these?? them?
You've confused me. :)
According to this your


would indicate that it is going to work at a constant speed at all times. Hence this is only going to work on 1 dimension (the horizontal plain.) Wings Levelled flight characteristics.

This is just going to be providing vertical lift capability, However it would be interesting to note that there is no mention on how to compensate in case of any other force i.e engine failure, strong winds, unstable pitch due to many atmospheric conditions.

One must also not undermine that lift is produce by relative wind speed that allows an aircraft to glide, just before landing there is ground effect which is normally calculated to be at almost half the wing length. In VTOL this does not exist.

Well I might be wrong but as far as I know its the INS which has the larger role to play, each INS has 3 accelerators and 3 ring laser gyroscopes and they 're oriented along each of the three axis (x,y,z) of the airplane, so it does consider all the 3 dimensions.Initially only a coarse vertical is established. And once vertical is established, the laser gyro senses earth rate components, which are used to establish the heading of the airplane. As the alignment continues, both the vertical reference and the heading determinations are fine tuned for maximum accuracy.
And its the software that does all the computations, including compensations, navigational calculations, and coordinate transformations. Gyro and accelerometer outputs are compensated for sensor bias, scale factor, misalignment, and thermal changes. The compensated signals are used in computing airplane pitch, roll and heading relative to the local navigation coordinates.
The inertial system display unit (ISDU) provides pilot interface with the Inertial reference units. The display of track angle, ground speed, present position, wind direction and speed, heading and system status is available in ISDU.
 
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