Attitude estimation for spin-stabilised projectiles is critical to modern guidance and control systems, ensuring precision in both military and civilian applications. Over the past decades, methods ...
Attitude estimation refers to the determination of an object’s orientation in three‐dimensional space, a core requirement for inertial navigation and measurement systems. Modern approaches rely on ...
A spacecraft attitude kinematics model, attitude measurement model, and filter algorithm are three important parts in spacecraft attitude determination, and a high-precision filtering algorithm is the ...
Some results have been hidden because they may be inaccessible to you
Show inaccessible results