Darin Koblick

Last seen: 2 months 前 | 自 2010 起处于活动状态

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Astrodynamicist and mathematician by trade

统计学

排名
320 of 20,554

声誉
4,788

平均
4.60

贡献数
31 文件

下载次数
141

ALL TIME 下载次数
44822

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Feeds

已提交

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

4 months 前 | 2 次下载 |

0.0 / 5

已提交

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

2 years 前 | 3 次下载 |

0.0 / 5

已提交

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

4 years 前 | 1 次下载 |

0.0 / 5

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

4 years 前 | 9 次下载 |

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.

4 years 前 | 1 次下载 |

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 ...

5 years 前 | 2 次下载 |

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...

6 years 前 | 1 次下载 |

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

8 years 前 | 4 次下载 |

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

9 years 前 | 5 次下载 |

0.0 / 5

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

9 years 前 | 2 次下载 |

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

10 years 前 | 1 次下载 |

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

11 years 前 | 2 次下载 |

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

11 years 前 | 4 次下载 |

5.0 / 5

已提交

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

11 years 前 | 16 次下载 |

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

12 years 前 | 18 次下载 |

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.

12 years 前 | 1 次下载 |

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.

12 years 前 | 10 次下载 |

5.0 / 5

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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.

13 years 前 | 2 次下载 |

0.0 / 5

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

13 years 前 | 3 次下载 |

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

13 years 前 | 2 次下载 |

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

13 years 前 | 1 次下载 |

5.0 / 5

已提交

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

13 years 前 | 6 次下载 |

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

13 years 前 | 2 次下载 |

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.

13 years 前 | 5 次下载 |

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

13 years 前 | 6 次下载 |

5.0 / 5

已提交

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

13 years 前 | 3 次下载 |

5.0 / 5

已提交

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

14 years 前 | 1 次下载 |

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

14 years 前 | 2 次下载 |

4.5 / 5

已提交

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

15 years 前 | 13 次下载 |

5.0 / 5

已提交

Convert Right Ascension and Declination to Azimuth and Elevation
Algorithm will convert topocentric RA/DEC Angles to Azimuth and Elevation

15 years 前 | 3 次下载 |

5.0 / 5

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