Aas 11-117 Distributed Orbit Determination via Estimation Consensus

نویسندگان

  • Ran Dai
  • Unsik Lee
  • Mehran Mesbahi
چکیده

This paper proposes an optimal algorithm for distributed orbit determination by using discrete observations provided from multiple tracking stations in a connected network. The objective is to increase the precision of estimation by communication and cooperation between tracking stations in the network. We focus on the dynamical approach considering a simplified Low Earth Orbital Satellite model with random perturbations introduced in the observation data which is provided as ranges between tracking stations and satellite. The dual decomposition theory associated with the subgradient method is applied here to decompose the estimation task into a series of suboptimal problems and then solve them individually at each tracking station to achieve the global optimality.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Aas 11-502 Gravity Error Compensation Using Second-order Gauss-markov Processes

Earth science satellite missions currently require orbit determination solutions with position accuracies to within a centimeter. The estimation of empirical accelerations has become commonplace in precise orbit determination (POD) for Earth-orbiting satellites. Dynamic model compensation (DMC) utilizes an exponentially time-correlated system noise process, known as a first-order GaussMarkov pr...

متن کامل

IAA-AAS-DyCoSS2 14-05-01 AN HEURISTIC APPROACH TO THE PROBLEM OF INITIAL ORBIT DETERMINATION: A TEST CASE WITH GEO OBSERVATIONS

The orbit determination of a satellite in a geostationary orbit is usually based on optical observations. Telescopes all around the Earth are observing the geostationary ring to obtain periodically new measurements in order to update the estimation of the objects’ orbits. One critical aspect of the orbit determination process is the initial orbit determination because no a priori information ar...

متن کامل

(Preprint) AAS INACTIVE SPACE OBJECT SHAPE ESTIMATION VIA ASTROMETRIC AND PHOTOMETRIC DATA FUSION

This paper presents a method to determine the shape of a space object in orbit while simultaneously recovering the observed space object’s inertial orientation and trajectory. This work studies a shape estimation approach based on octant triangulation applied to light curve and angles data fusion. The filter employs the Unscented estimation approach, reducing passively-collected electro-optical...

متن کامل

(Preprint) AAS NONLINEAR SEQUENTIAL METHODS FOR IMPACT PROBABILITY ESTIMATION

Orbit determination in application to the estimation of impact probability has the goal of determining the evolution of the state probability density function (pdf) and determining a measure of the probability of collision. Nonlinear gravitational interaction and non-conservative forces can make the pdf far from Gaussian. This work implements three nonlinear sequential estimators: the Extended ...

متن کامل

Aas 16-236 Probabilistic Initial Orbit Determination

Future space surveillance requires dealing with uncertainties directly in the initial orbit determination phase. We propose an approach based on Taylor differential algebra to both solve the initial orbit determination (IOD) problem and to map uncertainties from the observables space into the orbital elements space. This is achieved by approximating in Taylor series the general formula for pdf ...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2011