oygx210 Goto Github PK

eom

Equations of Motion for Astrodynamics

ephemeris

NASA JPL Planetary Ephemeris Export Package

ephemeris-compute-de405

A command-line tool for producing tables of the positions of solar system objects over time.

ephemeris-compute-de430

A command-line tool for producing tables of the positions of solar system objects over time.

ephemeris_generic_example

An example of ephemeris calculation with different toolkits and sources: NASA/NAIF SPICE toolkit with JPL DE430 ephemeris and also IAA RAS EPM 2017 ephemeris

epigraph

A C++ interface to formulate and solve linear, quadratic and second order cone problems.

eps

EPS related code (Matlab, STK, etc)

erfa

Essential Routines for Fundamental Astronomy. Maintainers: @eteq @mhvk @sergiopasra

esatadcs

Software for Theia Space's ESAT Attitude Determination and Control Subsystem

esatcom

ESAT's communications subsystem (COM) and ground station (GS) software.

esatobc

Software for Theia Space's ESAT On-Board Computer

eskf-attitude-estimation

Error-State KF algorithm to estimate attitude

esn

Application of echo state network (ESN) for the nonlinear control of a fixed-wing unmanned aerial vehicle (UAV)

esoq2

EStimation of Optimal Quaternion

etl

Embedded Template Library

example_sgp4

An example using David Vallado's Astrodynamics Software in an Octave workspace

examples-in-feedback-passivation-of-linear-systems-with-fixed-structured-controllers

exceloperation

excel操作类，封装了一些excel基本操作，包括：文件打开、关闭操作，数据读取、写入操作，文件保存及另存pdf操作等

extended-kalman-filter

Matlab and C++ code for implementation of the Extended Kalman Filter for estimating dynamic quantities for a single rigid body with distributed force/torque measurements and distributed gyroscopes and accelerometers measurements.It also include estimation of the orientation under the quaternion representation.

extended_state_observer

a disturbance rejection-based solution to the problem of robust output regulation of linear systems. The difference between the underlying plant and its nominal mathematical model is represented by two classes of disturbances. The first class is generated by an autonomous linear system while the other class has no specific dynamical structure. Robustness against the first disturbance class is achieved by the internal model principle. Next, in the framework of disturbance rejection control, an extended state observer (ESO) is designed to estimate and compensate for the second class of disturbances. As a result, the proposed output regulation method can deal with a vast range of uncertainties. The stability of the closed loop system is investigated and results on practical regulation are drawn. Keywords—Output regulation, extended state observer, disturbance rejection, linear system, robustness

exudyn

Flexible Multibody Dynamics Simulation with Python and C++

f16-flight-control-and-simulation

Nonlinear and linear flight simulation with autopilots for altitude hold, velocity hold, and pitch controls(SAS damper).

fadapt

Adaptive filter algorithms package for Matlab

fast-svd-wahba

Optimal Attitude Determination Algorithm Using Fast Singular Value Decomposition

fatrop

Fatrop is a nonlinear optimal control problem solver that aims to be fast, support a broad class of optimal control problems and achieve a high numerical robustness.

fault-ddpg

Fault-tolerant Control System using DDPG for a two-link manipulator

fcs_project

fdcl-hdf5

HDF5 wrapper for use with Eigen

feedback-doc

Desensitized Optimal Control using Feedback Control Design

fex-keplerstm