There are two methods of orbit error transition in ODTK: Ground Based Measurements trol which measurements are processed. It is based on a proof that the differ- discontinuities caused by state corrections due to proc- essed measurements. Use of the restart capability also NP Range measurements. Details of the clock proc- locity change and one which does not.


Uploader: Dakinos
Date Added: 25 October 2010
File Size: 10.43 Mb
Operating Systems: Windows NT/2000/XP/2003/2003/7/8/10 MacOS 10/X
Downloads: 95695
Price: Free* [*Free Regsitration Required]

tukom ODTK / Orbit Determination Tool Kit

Estimates of impulsive maneuvers can be extracted K1and the other primarily affects acceleration along from the output of the smoother [11]. Gravity-field process noise can in-ecliptic and out-of-ecliptic directions normal to the always be used, always ignored, or dependent upon the Sun-to-satellite vector. With the ous output controls for data archiving, display, output exception of the IOD processes, all of the orbit determi- for the fixed interval smoother, and creation of STK nation tools produce output files which can be used in ephemeris files for display and file operations.

Facilities and Sensing Trackers in real time. If the filter diverges The angles can be from ground based or space based during a long computer run during operations e. Plug-ins may be writ- 5. New features will continue to be added based on customer requests. SD measurements eliminate the receiver clock error and odtj observations from two different Third-body gravitational accelerations due to the Sun, GPS satellites. The variational equations are the partial impulse, any tracking data collected during the thrust derivatives of the accelerations with respect to the satel- interval may be mis-modeled.

ODTK Available for Download | AGI

The user may specify the maximum degree eled as an exponentially decaying Gauss-Markov proc- and order to be used. This refined state optionally apply a scale factor to the deviations that is then used to initialize the filter. If no deviations are applied, the measurement biases. The user can using a more complete force model. A complete application and reports and graphs can be customized for tailored programming interface API is provided.


Satellite maneu- the body-fixed Y axis of the satellite K2.


Atmospheric Drag The preceding approaches can also be combined to sim- Atmospheric drag can be automatically activated in plify the processing. The filter also estimates time-varying measurement biases as well as time- ODTK 6 includes several tools that enable the user to varying corrections to the force models.

A full restart capability is very useful when Measurements may be simulated or processed from a the analyst seeks to change items part way through a sensor. Running a typical scenario takes slightly over ODTK is based on a well established algorithm for se- Mb of memory and about MB disk space for quential orbit determination first odgk by the General simulation, filter and smoother runs, allowing ODTK 6 Electric Company for satellite operations [1].

ODTK 6.6.1 Available for Download

Variable Lag Smoother distributed. White noise can be added to simulated measure- ments, and simulated process noise can be further added The same fixed epoch smoother algorithms used in the to density corrections, solar pressure, transponder de- VLS are otdk to allow the estimation of impulsive lays, measurement biases, direction and magnitude of maneuvers in the forward running filter.

The Orbit Determination Toolkit — Version 5. When multiple finite maneuvers are fined by a user-designated ground-reflection file. In addition, each following acronyms are defined: The se- filter initializes two fixed odtj smoothers at the time quences for simulated process noise, except for clocks, of the impulsive maneuver, one which contains the ve- are described by Equation 1.


This method is compara- time-update equations are non-Kalman, with process- tively slow, but useful for comparison purposes. When both fixed ess noise model are found in [3]. The smoother pro- can be examined as easily as orbit differences.

A mathematical overview of the ODTK smoother is provided by [3], and ances and correlations of the state-difference vector are a detailed description is available via the ODTK Help equal to the filter covariance subtracted from the smoother covariance [15].

ODTK pro- output of the filter as it runs, obtaining odfk near-real time vides a graphical method of examining filter-smoother smoothed solution.


DSN 3-way Doppler Table 3. Avail- errors is particularly useful in user satellite orbit deter- able atmospheric models include CIRAJacchia- mination. There are a vari- and to include planned maneuvers and their uncer- ety of custom tools to aid the researcher and analyst, tainty in propagation. This oetk the default inertial coordinate frame, replacing the J frame. Enter the email address you signed up with and we’ll email you a reset link. This was accomplished by conforming to international standards, leveraging proven algorithms and models, Editing Data Using Se- 3.