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Proceedings ArticleDOI

A complementary filter for attitude estimation of a fixed-wing UAV

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TLDR
A nonlinear complementary filter is proposed that combines accelerometer output for low frequency attitude estimation with integrated gyrometer output for high frequency estimation that is evaluated against the output from a full GPS/INS that was available for the data set.
Abstract
This paper considers the question of using a nonlinear complementary filter for attitude estimation of fixed-wing unmanned aerial vehicle (UAV) given only measurements from a low-cost inertial measurement unit. A nonlinear complementary filter is proposed that combines accelerometer output for low frequency attitude estimation with integrated gyrometer output for high frequency estimation. The raw accelerometer output includes a component corresponding to airframe acceleration, occurring primarily when the aircraft turns, as well as the gravitational acceleration that is required for the filter. The airframe acceleration is estimated using a simple centripetal force model (based on additional airspeed measurements), augmented by a first order dynamic model for angle-of-attack, and used to obtain estimates of the gravitational direction independent of the airplane manoeuvres. Experimental results are provided on a real-world data set and the performance of the filter is evaluated against the output from a full GPS/INS that was available for the data set.

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Visual-inertial navigation, mapping and localization: A scalable real-time causal approach

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Keeping a Good Attitude: A Quaternion-Based Orientation Filter for IMUs and MARGs

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Patent

Unmanned aerial vehicle and operations thereof

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A Linear Kalman Filter for MARG Orientation Estimation Using the Algebraic Quaternion Algorithm

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References
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Book

Aircraft Control and Simulation

TL;DR: Equations of Motion Building the Aircraft Model Basic Analytical and Computational Tools Aircraft Dynamics and Classical Design Techniques Modern Design Techniques Robustness and Multivariable Frequency-Domain Techniques Digital Control Appendices Index.
Journal ArticleDOI

Nonlinear Complementary Filters on the Special Orthogonal Group

TL;DR: An observer on SO(3), termed the explicit complementary filter, that requires only accelerometer and gyro outputs; is suitable for implementation on embedded hardware; and provides good attitude estimates as well as estimating the gyro biases online.
Journal ArticleDOI

Survey of nonlinear attitude estimation methods

TL;DR: A survey of modern nonlinear filtering methods for attitude estimation based on the Gaussian assumption that the probability density function is adequately specified by its mean and covariance is provided.
Journal ArticleDOI

Novel quaternion Kalman filter

TL;DR: In this paper, the attitude-quaternion and gyro random drifts from vector measurements are estimated using a Kalman filter, and the covariance matrices of the system state-dependent noises are derived.
Journal ArticleDOI

A globally convergent angular velocity observer for rigid body motion

TL;DR: In this article, a novel angular velocity/angular momentum observer for rigid body motion is presented, and it is shown that the observer estimates converge globally and that the convergence is eventually exponential.
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