TL;DR: In this article, the authors present a dictionary of symbols for modeling the atmosphere, including equations of motion, coordinate and time systems, and initial orbit determination and estimation, as well as various perturbation techniques.
Abstract: 1. Equations of Motion. 2. Kepler's Equation and Kepler's Problem. 3. Coordinate and Time Systems. 4. Observations. 5. Celestial Phenomena. 6. Orbital Maneuvering. 7. Initial Orbit Determination. 8. Special Perturbation Techniques. 9. General Perturbation Techniques. 10. Orbit Determination and Estimation. 11. Mission Analysis. Appendix A: Dictionary of Symbols. Appendix B: Modeling the Atmosphere. Appendix C: Mathematical Fundamentals. Appendix D: Constants and Expansions.
TL;DR: In this paper, the authors present a review of matrix concepts for near-circular orbits and propose a solution of the linearized Equations of Motion (LEM) problem.
Abstract: 1 Orbit Determination Concepts 2 The Orbit Problem 3 Observations 4 Fundamentals of Orbit Determination 5 Square-root Solution Methods 6 Consider Covariance Analysis A Probability and Statistics B Review of Matrix Concepts C Equations of Motion D Constants E Analytical Theory for Near-Circular Orbits F Example of State Noise and Dynamic Model Compensation G Solution of the Linearized Equations of Motion H ECI and ECF Transformation
TL;DR: The German small satellite CHAMP is on the final track for launch on July 15, 2000 into a circular, near-polar and 460 km altitude orbit as discussed by the authors, with synergetic use for precise orbit determination, global gravity and magnetic field recovery, and GPS atmosphere and ionosphere profiling.
TL;DR: In this paper, the authors proposed a new method for fixing dual-frequency GPS ambiguities on undifferenced phase measurements either locally or globally, which can be used for precise point positioning of ground-based receivers and for precise orbit determination of low Earth orbiting satellites.
Abstract: Integer ambiguity fixing is routinely applied to double-differenced GPS phase measurements to achieve precise positioning. Double-differencing is interesting because it removes most of the common errors between the different signal paths. However, if common errors can be estimated it becomes attractive to fix integer ambiguities on undifferenced measurements. Phase measurements then become pseudorange-like measurements with a noise level of a few millimeters.
This paper introduces a new method for fixing dual-frequency GPS ambiguities on undifferenced phase measurements either locally or globally. The clocks for the GPS constellation obtained during this process can be used for precise point positioning of ground based receivers and for precise orbit determination of low Earth orbiting satellites. The resulting positioning precision is comparable to that of standard differential positioning without the need for a reference station. Ambiguity-fixed satellite orbits for the GRACE and Jason satellites are more precise than the most precise solution available today.
TL;DR: This work presents an ambiguity resolution algorithm that improves solution accuracy for single receiver point-positioning users and constrain (rather than fix) linear combinations of local phase biases to improve compatibility with global phase bias estimates.
Abstract: Global positioning system (GPS) data processing algorithms typically improve positioning solution accuracy by fixing double-differenced phase bias ambiguities to integer values. These “double-difference ambiguity resolution” methods usually invoke linear combinations of GPS carrier phase bias estimates from pairs of transmitters and pairs of receivers, and traditionally require simultaneous measurements from at least two receivers. However, many GPS users point position a single local receiver, based on publicly available solutions for GPS orbits and clocks. These users cannot form double differences. We present an ambiguity resolution algorithm that improves solution accuracy for single receiver point-positioning users. The algorithm processes dual- frequency GPS data from a single receiver together with wide-lane and phase bias estimates from the global network of GPS receivers that were used to generate the orbit and clock solutions for the GPS satellites. We constrain (rather than fix) linear combinations of local phase biases to improve compatibility with global phase bias estimates. For this precise point positioning, no other receiver data are required. When tested, our algorithm significantly improved repeatability of daily estimates of ground receiver positions, most notably in the east component by approximately 30% with respect to the nominal case wherein the carrier biases are estimated as real values. In this “static” test for terrestrial receiver positions, we achieved daily repeatability of 1.9, 2.1 and 6.0 mm in the east, north and vertical (ENV) components, respectively. For kinematic solutions, ENV repeatability is 7.7, 8.4, and 11.7 mm, respectively, representing improvements of 22, 8, and 14% with respect to the nominal. Results from precise orbit determination of the twin GRACE satellites demonstrated that the inter-satellite baseline accuracy improved by a factor of three, from 6 to 2 mm up to a long-term bias. Jason-2/Ocean Surface Topography Mission precise orbit determination tests results implied radial orbit accuracy significantly below the 10 mm level. Stability of time transfer, in low-Earth orbit, improved from 40 to 7 ps. We produced these results by applying this algorithm within the Jet Propulsion Laboratory’s (JPL’s) GIPSY/OASIS software package and using JPL’s orbit and clock products for the GPS constellation. These products now include a record of the wide-lane and phase bias estimates from the underlying global network of GPS stations. This implies that all GIPSY–OASIS positioning users can now benefit from this capability to perform single-receiver ambiguity resolution.