Youn et al., 2019 - Google Patents
Fuzzy adaptive attitude estimation for a fixed-wing UAV with a virtual SSA sensor during a GPS outageYoun et al., 2019
- Document ID
- 17706860480996405393
- Author
- Youn W
- Rhudy M
- Cho A
- Myung H
- Publication year
- Publication venue
- IEEE Sensors Journal
External Links
Snippet
This paper proposes a novel robust attitude estimation algorithm for a small unmanned aerial vehicle (UAV) in the absence of GPS measurements. A synthetic sideslip angle (SSA) measurement formulated for use under the zeroangle assumption is newly proposed for a …
- 230000003044 adaptive 0 title abstract description 20
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
- 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
- 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
-
- 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
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
-
- 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
- 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
- G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
- G05D1/0044—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement by providing the operator with a computer generated representation of the environment of the vehicle, e.g. virtual reality, maps
-
- 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
- G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed, acceleration
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Youn et al. | Fuzzy adaptive attitude estimation for a fixed-wing UAV with a virtual SSA sensor during a GPS outage | |
Youn et al. | Combined quaternion-based error state Kalman filtering and smooth variable structure filtering for robust attitude estimation | |
Fontanella et al. | MEMS gyros temperature calibration through artificial neural networks | |
Madyastha et al. | Extended Kalman filter vs. error state Kalman filter for aircraft attitude estimation | |
Guo et al. | Multisensor data-fusion-based approach to airspeed measurement fault detection for unmanned aerial vehicles | |
Mahony et al. | Nonlinear complementary filters on the special orthogonal group | |
Wenz et al. | Moving horizon estimation of air data parameters for UAVs | |
Sikkel et al. | A novel online model-based wind estimation approach for quadrotor micro air vehicles using low cost MEMS IMUs | |
Wu et al. | A novel approach for attitude estimation based on MEMS inertial sensors using nonlinear complementary filters | |
Youn et al. | Accelerometer fault-tolerant model-aided state estimation for high-altitude long-endurance UAV | |
CN102692225A (en) | Attitude heading reference system for low-cost small unmanned aerial vehicle | |
Kang et al. | A human motion tracking algorithm using adaptive EKF based on Markov chain | |
No et al. | Attitude estimation method for small UAV under accelerative environment | |
Leutenegger et al. | Robust state estimation for small unmanned airplanes | |
Baldwin et al. | A nonlinear observer for 6 DOF pose estimation from inertial and bearing measurements | |
Chang et al. | A two-step approach for an enhanced quadrotor attitude estimation via IMU data | |
Youn et al. | Aerodynamic model-aided estimation of attitude, 3-D wind, airspeed, AOA, and SSA for high-altitude long-endurance UAV | |
Castellanos et al. | A low-cost air data attitude heading reference system for the tourism airplane applications | |
Lim et al. | Deep learning-aided synthetic airspeed estimation of UAVs for analytical redundancy with a temporal convolutional network | |
Youn | Magnetic fault–tolerant navigation filter for a UAV | |
Youn et al. | Model-aided synthetic airspeed estimation of UAVs for analytical redundancy | |
Oh | Multisensor fusion for autonomous UAV navigation based on the Unscented Kalman Filter with Sequential Measurement Updates | |
Condomines et al. | Pi-invariant unscented Kalman filter for sensor fusion | |
Lyu et al. | A model-aided optical flow/inertial sensor fusion method for a quadrotor | |
Weibel et al. | Small unmanned aerial system attitude estimation for flight in wind |