Tsukerman et al., 2017 - Google Patents
Analytic evaluation of fine alignment for velocity aided INSTsukerman et al., 2017
- Document ID
- 16790257793868840541
- Author
- Tsukerman A
- Klein I
- Publication year
- Publication venue
- IEEE Transactions on Aerospace and Electronic Systems
External Links
Snippet
Coarse attitude initialization procedure is used to determine the initial attitude of the inertial navigation system. To improve the accuracy of the attitude to a desired value, fine alignment (FA) process is employed. In stationary conditions, zero velocity updates are usually used to …
- 238000011156 evaluation 0 title abstract description 12
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/10—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/165—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/53—Determining attitude
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/20—Instruments for performing navigational calculations
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments and devices referred to in the preceding groups
- G01C25/005—Manufacturing, calibrating, cleaning, or repairing instruments and devices referred to in the preceding groups initial alignment, calibration or starting-up of inertial devices
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/34—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
- G01C19/38—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Tsukerman et al. | Analytic evaluation of fine alignment for velocity aided INS | |
| CN105737828B (en) | A kind of Combinated navigation method of the joint entropy Extended Kalman filter based on strong tracking | |
| Crocoll et al. | Model‐aided navigation for a quadrotor helicopter: A novel navigation system and first experimental results | |
| CN110988926B (en) | Method for realizing position accurate fixed point deception migration in loose GNSS/INS combined navigation mode | |
| Luo et al. | A position loci-based in-motion initial alignment method for low-cost attitude and heading reference system | |
| Xue et al. | In-motion alignment algorithm for vehicle carried sins based on odometer aiding | |
| Ben et al. | A dual-state filter for a relative velocity aiding strapdown inertial navigation system | |
| Stančić et al. | The integration of strap-down INS and GPS based on adaptive error damping | |
| CN114061575A (en) | Missile attitude angle fine alignment method and system under condition of large misalignment angle | |
| Ali et al. | Performance comparison among some nonlinear filters for a low cost SINS/GPS integrated solution | |
| Kaygısız et al. | In-motion alignment of a low-cost GPS/INS under large heading error | |
| Shabani et al. | Improved underwater integrated navigation system using unscented filtering approach | |
| Klein et al. | INS fine alignment with low-cost gyroscopes: Adaptive filters for different measurement types | |
| Lee et al. | Trajectory estimation of reentry vehicles by use of on-line input estimator | |
| RU2654964C1 (en) | Method for determining of adjustment corrections in the strap down inertial navigation system | |
| Gong et al. | Airborne earth observation positioning and orientation by SINS/GPS integration using CD RTS smoothing | |
| Klein et al. | Squeezing position updates for enhanced estimation of land vehicles aided INS | |
| Li et al. | Velocimeter-aided attitude estimation for Mars autonomous landing: Observability analysis and filter algorithms | |
| Bashir et al. | Kalman Filter Based Sensor Fusion for Altitude Estimation of Aerial Vehicle | |
| Crain et al. | Mars entry navigation: atmospheric interface through parachute deploy | |
| Lemay et al. | Precise input and output error characterization for loosely integrated ins/gps/camera navigation system | |
| Klein et al. | Comparison between adaptive extended Kalman filters for INS accurate fine alignment process | |
| Ben-Ishai et al. | Kalman filter mechanization in INS/Seeker fusion and observability analysis | |
| Klein et al. | Assessment of aided-INS performance | |
| Tsukerman et al. | Analytic steady-state solution of fine alignment with velocity measurements |