Space flight tests of attitude determination using GPS

Abstract

Preliminary space flight results of attitude determination using GPS are presented from a spacecraft in low Earth orbit. Relative position measurements accurate to the sub‐centimetre level are made among multiple GPS antennas mounted on the space vehicle. A Trimble Navigation TANS Quadrex (a GPS receiver specially adapted for attitude determination by Stanford University) is used as a differential carrier phase sensor for the flight. Four GPS antennas are mounted on the zenith face of RADCAL, a polar orbiting, gravity‐gradient‐stabilized Air Force Space Test Program Satellite, built by Defense Systems, Inc. The four antennas are equally spaced about the perimeter of the 30 inch diameter cylindrical spacecraft bus. The Quadrex receiver measures the phase of the L‐band GPS carrier (1575 MHz) at each of up to four antennas for up to six GPS satellites simultaneously. From these measurements, an initial assessment of attitude determination in space is performed in post‐processing. For RADCAL, the attitude solution is greatly overdetermined. In a preliminary evaluation of system performance, the system accuracy is determined through measurement self‐consistency. Analysis of the attitude motion in the context of a gravity gradient dynamic model yields further insight into the system performance.

Rigid Body Localization Using Sensor Networks

“…Substituting (2) in (11), we arrive at the following linear model (13) which can then be vectorized to (14) where is the unknown parameter vector that has to be estimated. The covariance matrix of the noise in (14) is denoted by where is the covariance matrix of , and is developed in Appendix A.…”

Improving the GNSS Attitude Ambiguity Success Rate with the Multivariate Constrained LAMBDA Method

“…Many works investigated the feasibility and performance of GNSS Attitude Determination, see e.g. [1][2][3][4][5][6]. The key for a precise attitude estimation is the ambiguity resolution process, since only when the integers inherent to the GNSS carrier phase observations are correctly fixed one is able to exploit the carrier phase data, which are of two orders of magnitude more accurate than the GNSS code observations.…”

A Robust GPS Receiver Self Survey Algorithm

“…Using a GPS receiver with pseudorange measurements, instantaneous positions as well as precise time can be determined [1]. In addition, a GPS receiver has the ability to provide attitude information by employing multiple antenna sets to measure the signal carrier phase differences [2][3][4][5]. However, when using the phase measurements the solution becomes more complicated than position determination since the phase measurements contain integer ambiguities [6][7][8].…”