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GRACE GRAVITY FIELD SOLUTIONS USING THE DIFFERENTIAL GRAVIMETRY APPROACH M. Weigelt, W. Keller

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Geophysical implications of the gravity field Geodesy Continental Hydrology Oceano- graphy Glacio- logy Atmosphere Tides Earth core Solid Earth Geoid 2

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Geophysical implications of the gravity field 3 ESA

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Observation system 4 GRACE = Gravity Recovery and Climate Experiment Initial orbit height: ~ 485 km Inclination: ~ 89 Key technologies: GPS receiver Accelerometer K-Band Ranging System Observed quantity: range range rate CSR, UTexas

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Gravity field modelling 5 with gravitational constant times mass of the Earth radius of the Earth spherical coordinates of the calculation point Legendre function degree, order (unknown) spherical harmonic coefficients

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Spectral representations 6 Spherical harmonic spectrum Degree RMS

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Outline GRACE geometry Solution strategies Variational equations Differential gravimetry approach What about the Next-Generation-GRACE? 7

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Geometry of the GRACE system

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9 B A Differentiation Integration Rummel et al. 1978

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Solution Strategies

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Solution strategies 11 Variational equationsIn-situ observations Classical (Reigber 1989, Tapley 2004) Celestial mechanics approach (Beutler et al. 2010, Jggi 2007) Short-arc method (Mayer-Grr 2006) Energy Integral (Han 2003, Ramillien et al. 2010) Differential gravimetry (Liu 2010) LoS Gradiometry (Keller and Sharifi 2005) Numerical integration Analytical integration

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Equation of motion 12 Basic equation: Newtons equation of motion where are all gravitational and non-gravitational disturbing forces In the general case: ordinary second order non-linear differential equation Double integration yields:

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Linearization 13 For the solution, linearization using a Taylor expansion is necessary: Types of partial derivatives: initial position initial velocity residual gravity field coefficients additional parameter Homogeneous solution Inhomogeneous solution

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Homogeneous solution 14 Homogeneous solution needs the partial derivatives: Derivation by integration of the variational equation Double integration !

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Inhomogeneous solution (one variant) 15 Solution of the inhomogeneous part by the method of the variation of the constant (Beutler 2006): with being the columns of the matrix of the variational equation of the homogeneous solution at each epoch. Estimation of by solving the equation system at each epoch:

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Application to GRACE 16 In case of GRACE, the observables are range and range rate: Chain rule needs to be applied:

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Limitations additional parameters compensate errors in the initial conditions counteract accumulation of errors outlier detection difficult limited application to local areas high computational effort difficult estimation of corrections to the initial conditions in case of GRACE (twice the number of unknowns, relative observation) 17

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In-situ observations: Differential gravimetry approach

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Instantaneous relative reference frame 19 PositionVelocity

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In-situ observation 20 Range observables: Multiplication with unit vectors: GRACE

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Relative motion between two epochs 21 absolute motion neglected! Epoch 1 Epoch 2 K-Band GPS

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Limitation 22 Combination of highly precise K-Band observations with comparably low accurate GPS relative velocity

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Residual quantities Orbit fitting using the homogeneous solution of the variational equation with a known a priori gravity field Avoiding the estimation of empirical parameters by using short arcs 23 true orbit GPS-observations estimated orbit

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Residual quantities 24 ratio 1:2 ratio 25:1

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Approximated solution 25

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Next generation GRACE

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27 New type of intersatellite distance measurement based on laser interferometry Noise reduction by a factor 10 expected M. Dehne, Quest

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Solution for next generation GRACE 28

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Variational equations for velocity term Reduction to residual quantity insufficient Modeling the velocity term by variational equations: Application of the method of the variations of the constants 29

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Results 30 Only minor improvements by incorporating the estimation of corrections to the spherical harmonic coefficients due to the velocity term Limiting factor is the orbit fit to the GPS positions additional estimation of corrections to the initial conditions necessary

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Summary The primary observables of the GRACE system (range & range rate) are connected to gravity field quantities through variational equations (numerical integration) or through in-situ observations (analytical integration). Variational equations pose a high computational effort. In-situ observations demand the combination of K-band and GPS information. Next generation GRACE instruments pose a challenge to existing solution strategies. 31