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Darin Koblick


Last seen: 18 giorni fa Attivo dal 2010

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Astrodynamicist and Founder of Coorbital Inc.

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  • GitHub Submissions Level 1
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Flatten Any Mulitdimensional Matrix into a 2-D Matrix!
Convert any multidimensional matrix into a 2-D Matrix. Then convert it back to its original form.

circa 2 mesi fa | 340 download |

0.0 / 5
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Yahoo Finance API (2025)
This is a simple way to use the Yahoo web API in MATLAB.

7 mesi fa | 409 download |

5.0 / 5
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chebyspace (Chebyshev Node Spacing)
Create a Chebyshev node spaced vector of n points between a and b.

oltre un anno fa | 21 download |

0.0 / 5
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Plotting Uncertainty (Bounded Line)
Display the upper and lower uncertainty bounds about X and Y datasets in a highly customizable style

quasi 4 anni fa | 289 download |

0.0 / 5
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KeplerMinMax
A novel closed-form solution to compute the surface altitude extrema for any two-body orbit

circa 5 anni fa | 15 download |

0.0 / 5
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Convert ECI to ECEF Coordinates
Transform ECI position, velocity and acceleration to ECEF position, velocity & acceleration.

quasi 6 anni fa | 6378 download |

4.2 / 5
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Calculate if an Angle is Between Two Angles
This routine will check whether an angle is contained between two other angles specifying lower and upper bounds.

quasi 6 anni fa | 57 download |

0.0 / 5
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Generate an Array of Random Strings
Want to generate a password with specific upper/lower case and wild character requirements? Perhaps quickly determine a unique ...

oltre 6 anni fa | 98 download |

0.0 / 5
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Peak and Threshold SNR given an Average False Alarm Rate
Determine the Peak SNR Needed to achieve a desired False Alarm Rate at a Specific Probability of Detection and pulse duration in...

oltre 7 anni fa | 100 download |

0.0 / 5
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Vectorized Multi-Dimensional Matrix Multiplication
Take Any N-D Matrix and Multiply it by another N-D Matrix Without a For-Loop

circa 9 anni fa | 851 download |

4.5 / 5
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Vectorized Orbital Decay Routine For Space Objects Between 180 and 500 km Altitude.
Fully vectorized routine will estimate the decay time for Earth orbiting objects

oltre 10 anni fa | 713 download |

0.0 / 5
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rotVecAroundArbAxis(unitVec2Rotate,rotationAxisUnitVec,theta)
Vectorized 3-D rotation of any vector around an arbitrary axis

circa 11 anni fa | 794 download |

5.0 / 5
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Vectorized Diagonal of any Multi-Dimensional Matrix
Given an N-D matrix, this routine will return the diagonal elements of any two dimensions

oltre 11 anni fa | 262 download |

5.0 / 5

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Parallel Implementation of the Picard Iteration For Linear BVP PDEs
Parallel Picard Iteration for a Linear Hyperbolic BVP PDE

oltre 12 anni fa | 344 download |

0.0 / 5
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Efficient Vector Rotation Matrix Routine
Efficient Method to Determine a Matrix Needed to Rotate One Vector to Another

oltre 12 anni fa | 615 download |

5.0 / 5

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Convert Keplerian Orbital Elements to a State Vector
Convert orbital elements to a state vector, or a state vector back to orbital elements.

oltre 12 anni fa | 4507 download |

4.5 / 5
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Vectorized Solar Azimuth and Elevation Estimation
Predict the topocentric solar position defined by geodetic lat, lon, Alt, and a universal time

oltre 13 anni fa | 6970 download |

4.6 / 5
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2000 ASTM Standard Extraterrestrial Spectrum Reference E-490-00
Vectorized MATLAB code which will compute the solar flux given a wave length.

oltre 13 anni fa | 558 download |

5.0 / 5
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Vectorized Clohessy-Wiltshire Hill Linear Propagation
A Demonstration of Linear Satellite Orbit Propagation Using Clohessy-Wiltshire Equations of Motion.

oltre 13 anni fa | 1870 download |

5.0 / 5
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Vectorized Picard-Chebyshev Method
Vectorized Picard-Chebyshev Method used for the analysis of the 2012 ASME Conference paper 87878

circa 14 anni fa | 733 download |

5.0 / 5
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State Vector Warping Routine
Calculate new ECI vectors corresponding to a desired time while fixing their relative earth position

circa 14 anni fa | 503 download |

3.0 / 5
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Convert Julian Date to Greenwich Apparent Sidereal Time
Find the Greenwich Apparent Sidereal Time Given any Julian Date

circa 14 anni fa | 1182 download |

5.0 / 5

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Gauss-Jackson Eighth-Order ODE Solver (Fixed Step Size)
Gauss-Jackson Eight-Order MultiStep Predictor-Corrector using ODE113 in its startup procedure.

oltre 14 anni fa | 949 download |

4.5 / 5
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Vectorized Analytic Two Body Propagator (Kepler Universal Variables)
Analytic propagation routine uses universal variables to solve a single formula for all orbit types

oltre 14 anni fa | 944 download |

3.0 / 5
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Convert ECEF to ECI Coordinates
Take any vector or series of vectors in the ECEF Coordinate frame and convert them to ECI.

oltre 14 anni fa | 4607 download |

3.8 / 5
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Convert UTC to Solar Apparent Time
Convert a time given in UTC to Solar Apparent or Solar Mean Time

quasi 15 anni fa | 1001 download |

5.0 / 5

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Equation of Time
Compute the equation of time with accuracy on the order of seconds.

quasi 15 anni fa | 691 download |

5.0 / 5
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Bulirsch-Stoer Propagator/Integrator
Implementation of the Bulirsch-Stoer algorithm for purposes of numerical orbit propagation.

oltre 15 anni fa | 1030 download |

0.0 / 5
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Lunar Azimuth and Altitude Estimation Algorithm
Predict the Lunar Azimuth and Altitude within +/- .2 deg of any lat and lon for a given UTC

quasi 16 anni fa | 3575 download |

4.5 / 5
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Julian Date to Greenwich Mean Sidereal Time
Convert a given Julian Date to Greenwich Mean Sidereal Time (GMST) in degrees.

circa 16 anni fa | 2092 download |

5.0 / 5

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