English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Plus monthly

Global: Zendy Tools annual

Global: Zendy Tools monthly

Global: Zendy Free Plan

This work presents a method for generating position, attitude, and velocitystates for an aircraft following a smoothed reference trajectory. The methodalso generates accelerometer and gyro measurements consistent with the aircraftstates. This work describes three corner smoothing algorithms for generating asmoothed reference trajectory from a series waypoints that accounts forlimitations in the physical system. The smoothed reference trajectory, andcurvilinear motion theory are used to generate the lower-order states. Acoordinated turn maneuver is then applied to generate accelerometer and gyromeasurement estimates.

Analytical Aircraft State and IMU Signal Generator from Smoothed Reference Trajectory