Correction to: Fundamentals of Spacecraft Attitude Determination and Control Page 1 Correction
to: Fundamentals of Spacecraft Attitude Determination and Control Correction to: FL Markley …

This study surveys the developments in the gyroless attitude determination system,
especially for small satellites. Two kinds of gyroless satellite attitude determination …

Descripción dele ditor:" The subject of integrated navigation systems covered in this book is
designed for those directly involved with the design, integration, and test and evaluation of …

The classical Fourier transform is one of the most widely used mathematical tools in
engineering. However, few engineers know that extensions of harmonic analysis to …

This paper presents a novel Kalman filter for the accurate determination of a vehicle's
attitude (pitch and roll angles) using a low-cost MEMS inertial measurement unit (IMU) …

New real-time approaches for three-axis magnetometer sensor calibration are derived.
These approaches rely on a conversion of the magnetometer-body and geomagnetic …

GNSS-based Attitude Determination (AD) of a mobile object using the readings of the Global
Navigation Satellite Systems (GNSS) is an active area of research. Numerous attitude …

In the normal operation conditions of a pico satellite, a conventional Unscented Kalman
Filter (UKF) gives sufficiently good estimation results. However, if the measurements are not …

This paper describes a novel low-cost inertial reference unit (IRU) developed for spin-
stabilized sounding rockets, as well as a method to calibrate the IRU using a one-axis rate …

Attitude motion of a satellite equipped with magnetic control system is considered. System
comprises of three magnetorquers and one three-axis magnetometer. Satellite is stabilized …