Simulation for spacecraft attitude control system analysis and design

全局路径后端平滑系列：基于apollo的分段spline平滑算法，使用osqp-eigen求解，通过matplotlib-cpp画图展示

Example code for "Maximum Reaction-wheel Array Torque/Momentum Envelopes for General Configurations."

Implementations of the major developments in 3D-attitude determination of spacecraft including the Triad method and various solutions to the Wahba's problem.

The Spacedyn is a library for the kinematic and dynamic analysis and simulation of articulated multi-body systems with a moving base written as MATLAB toolbox or C++ library. Examples of such syste…

spacecraft orbit calculate