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Description: ROVINS NANO merges the established high-grade iXBlue inertial navigation system with our competitive IMU. It is built on iXBlue's renowned FOG truly solid state technology and offshore instrumentation expertise. ROVINS NANO offers the unbeatable stability and accuracy of the inertial position whileShow More
Description: while simplifying the operation with its automatic and autonomous external sensor management. ROVINS NANO is the ROV navigation solution you can rely on, bringing an additional level of safety in case of deficient aiding sensors. Benefits Inertial position & velocity, available without DVL Open
- Angular Rate Range: 41.67 rpm
- Linear Acceleration Range: -5 to 5 +/-g
- Electrical Output: Pulse / Frequency, Serial / Digital
- Device Type: Optical
Inertial Navigation Systems - High Performance MEMS Subsea Motion Reference Unit -- Ekinox-M Subsea MRUSupplier: SBG Systems SAS
Description: Ekinox-M is an ITAR Free Subsea Motion Reference Unit (MRU) designed for subsea applications - Up to 6,000 m. It combines an Inertial Measurement Unit (IMU) and runs an enhanced on-board Extended Kalman Filter (EKF). High Performance for a Cost-effective Solution: 0.05° Attitude @ 200 Hz
- Linear Acceleration Range: 2 +/-g
- Electrical Output: Serial / Digital, Network / Fieldbus Output
- Linear Acceleration Measurement: MEMS
- Maximum Dimension: 6.1 inch
Description: stability theory for nonlinear control design; derivation of optimal control strategies via Pontryagin's maximum principle; and derivation of a local coordinate system. In navigation, the global positioning system (GPS) is described in detail, as are inertial navigation systems (INS), which are treatedShow More
Inertial Navigation Systems - LTN-101 FLAGSHIP GNADIRU - Global Navigation, Air Data, Inertial Reference UnitSupplier: Northrop Grumman Corporation
Description: The LTN-101 FLAGSHIP™ is an integrated global navigation, air data, inertial reference unit (GNADIRU). Introduced in 1992, FLAGSHIP™ has established an exceptional reliability record of over 16,000 operating hours MTBF on such leading commercial aircraft as the Airbus wide and narrowShow More
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Journal of Spacecraft and Rockets > Review of Options for Autonomous Cislunar Navigation
C. Sources of Autonomous Inertial Navigation Updates .
Bose-Einstein interferometry and its applications to precision undersea navigation
Current autonomous inertial navigation systems (INS) which are platform based or strapdown, , consist of accelerometers and gyros with the aid of Earth gravity maps and/or gradiometers, , , where each INS design could be application dependent.
Interpretation of acceleration measurements in inertial navigation
Abstract—It is shown that, when the absolute and apparent accelerations are measured simultaneously, the problem of autonomous inertial navigation is reduced to the solvable inverse problem.
Advances in Estimation, Navigation, and Spacecraft Control
This paper describes a loosely coupled approach for the improvement of state estimation in autonomous inertial navigation , using image-based rela- tive motion estimation for augmentation.
Algorithm for integrated inertial-satellite navigation systems
INTRODUCTION The autonomous inertial navigation systems (INSs) often fail to determine the navigation parameters of mobile objects with desired accuracy; therefore, the desired qualitative characteristics are achieved by integrating various navigation systems (NSs).
Identification of the state of a moving object by observation of geophysical fields
Usually, information about the object trajectory is given by the autonomous inertial navigation system.
sent solutions that would allow for autonomous inertial navigation updates.
A deep-sea drilling rig MEMS gyroscope random drift error correction method
In the field of marine technology, the use of autonomous inertial navigation system, real-time measurement of the current 3D pose of the carrier, is the main direction of the present study.
Handbook of Signal Processing Systems
Typically, the required performance for a navigation-grade system can be that the position error must not increase by more than one nautical mile (1.85 km) after one hour of autonomous inertial navigation .
Integrated inertial-satellite navigation system corrected with observations of a single star
Autonomous inertial navigation systems (INS) are intended for determining the position and spatial orientation of moving objects, but the instability of these systems inhibits their widespread use .
Aerobasics — An introduction to aeronautics
To counter this possibility, combat airplanes use a fully autonomous inertial navigation sys- tem (INS) which was originally developed for use in sub- marines.
Eurocopter AS 532UL Cougar Hélicoptère d'Observation Radar et d'Investigation sur ZONe (HORIZON) variant
… AGATHA datalink (see previously); an interface for the French Army's ATLAS artillery command, control, communications and intelligence system; a Multifunction Information Distribution System-Terre (MIDS-T) terminal (see Payloads) and a satellite communications capability an autonomous inertial navigation system that is updated …
Design of a Navigation Control by Information Criteria
For modeling the motion of the autonomous inertial navigation system, its parameters and measurers were chosen as follows: the coeﬃcients of platform drift Ri = 3 × 10−6 rad/s, Ui = 2 × 10−7 rad s/m, and Kij = 0; i, j = x, y, z.
TERMINAL GUIDANCE DEVELOPED FOR RUSSIAN BALLISTIC MISSILES
According to Solunin, this technique provided an accuracy an order of magnitude better than that of conventional autonomous inertial navigation systems.