Add to ORKGThis work presents a method for generating position, attitude, and velocity states for an aircraft following a smoothed reference trajectory. The method also generates accelerometer and gyro measurements consistent with the aircraft states. This work describes three corner smoothing algorithms for generating a smoothed reference trajectory from a series waypoints that accounts for limitations in the physical system. The smoothed reference trajectory, and curvilinear motion theory are used to generate the lower-order states. A coordinated turn maneuver is then applied to generate accelerometer and gyro measurement estimates
This paper presents an extended Kalman filter (EKF) for estimating the attitude and heading for guid...
A new approach towards the automated solution of realistic near-optimal aircraft trajectories is int...
We developed a signal processing algorithm to determine three components of the velocity vector of a...
This work presents a method for generating position, attitude, and velocity states for an aircraft f...
As world manufacturing technologies nowadays are transforming to industry revolution 4.0, autonomous...
An algorithm for aircraft trajectory prediction is presented that is based on two algebraic represen...
This thesis deals with attitude measurement by fusing sensor information from accelerometers, gyros ...
Aircraft trajectory generation is a widely addressed problem with applications including emergency t...
Abstract Using a synthesis algorithm of a linear state observer one estimates the state vector for ...
This article presents basic methodology and some algorithms for estimating attitude and heading angl...
DESIGN of maneuvers for carefree access of an aircraft to its complete flight envelope including pos...
The filter/smoother combination provides the most accurate means of trajectory reconstruction. Not a...
This thesis presents the flight trajectory analysis for a given aircraft configuration starting wit...
Aircraft flight test data are processed by optimal estimation programs to estimate the aircraft stat...
Abstract — In this paper we present a state estimation method based on an inertial measurement unit ...
This paper presents an extended Kalman filter (EKF) for estimating the attitude and heading for guid...
A new approach towards the automated solution of realistic near-optimal aircraft trajectories is int...
We developed a signal processing algorithm to determine three components of the velocity vector of a...
This work presents a method for generating position, attitude, and velocity states for an aircraft f...
As world manufacturing technologies nowadays are transforming to industry revolution 4.0, autonomous...
An algorithm for aircraft trajectory prediction is presented that is based on two algebraic represen...
This thesis deals with attitude measurement by fusing sensor information from accelerometers, gyros ...
Aircraft trajectory generation is a widely addressed problem with applications including emergency t...
Abstract Using a synthesis algorithm of a linear state observer one estimates the state vector for ...
This article presents basic methodology and some algorithms for estimating attitude and heading angl...
DESIGN of maneuvers for carefree access of an aircraft to its complete flight envelope including pos...
The filter/smoother combination provides the most accurate means of trajectory reconstruction. Not a...
This thesis presents the flight trajectory analysis for a given aircraft configuration starting wit...
Aircraft flight test data are processed by optimal estimation programs to estimate the aircraft stat...
Abstract — In this paper we present a state estimation method based on an inertial measurement unit ...
This paper presents an extended Kalman filter (EKF) for estimating the attitude and heading for guid...
A new approach towards the automated solution of realistic near-optimal aircraft trajectories is int...
We developed a signal processing algorithm to determine three components of the velocity vector of a...