Sentence examples for yaw attitude from inspiring English sources

We consider the problem of controlling the vertical, lateral, longitudinal and yaw attitude motion of a helicopter along desired arbitrary trajectories with only restrictions on the time derivatives imposed by the functional controllability of the system.

In this paper we design an autopilot in order to control the vertical, lateral, longitudinal and yaw attitude dynamic of an helicopter achieving a desired four degree of freedom trajectory.

The outer loop of the system provides pitch and roll attitude commands to the inner loop, which in turns generates the tilting angles that are required to control the quadrotor position in the horizontal inertial plane in addition to the required reaction torque and thrust for yaw attitude and altitude tracking, respectively.

The estimated horizontal antenna phase center offsets implicitly provide the spacecraft's yaw-attitude.

Whereas a lot of effort has been put in to examine the yaw-attitude control of GPS satellites that are in eclipsing orbits, hardly anything is known about the yaw-attitude behavior of eclipsing GLONASS-M satellites.

The insights gained from studying the yaw angle behavior have led to the development of the very first yaw-attitude model for eclipsing GLONASS-M satellites.

The derived yaw-attitude model proves to be much better than the nominal yaw-attitude model commonly being used by today's GLONASS-capable GNSS software packages as it reduces the observation residuals of eclipsing satellites down to the normal level of non-eclipsing satellites and thereby prevents a multitude of measurements from being incorrectly identified as outliers.

The proper modeling of the satellites' yaw-attitude is a prerequisite for high-precision Global Navigation Satellite System (GNSS) positioning and poses a particular challenge during periods when the satellite orbital planes are partially eclipsed.

The designed controllers can efficiently control the roll, pitch and yaw satellite attitudes.

Building up on previous research for spacecraft in yaw-steering (YS) attitude, analytical expressions for the SRP acceleration in orbit-normal (ON) attitude are established based on a generic box-wing model, and related to the corresponding parameters of the ECOM.

The first breakthrough occurred in the domain of sensors for position, speed, acceleration, and attitude (yaw, pitch, roll) measurements.