Quaternion‐Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach
H Septanto, RT Bambang… - … and Simulation in …, 2014 - Wiley Online Library
It is well known that single equilibrium orientation point in matrix rotation is represented by
two equilibrium points in quaternion. This fact would imply nonefficient control effort as well …
two equilibrium points in quaternion. This fact would imply nonefficient control effort as well …
[PDF][PDF] Research Article Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach
It is well known that single equilibrium orientation point in matrix rotation is represented by
two equilibrium points in quaternion. This fact would imply nonefficient control effort as well …
two equilibrium points in quaternion. This fact would imply nonefficient control effort as well …
[PDF][PDF] HARRY SEPTANTO"", BAMBANG RIYANTO TRILAKSONO", ARIEF SYAICHU-ROHMAN
RE PoETRO, ARA IBRAHIM - researchgate.net
This paper proposes a novel nonlinear continuous quaternion-based attitude control system
composing augmented dynamic that guaranteed to be able to regulate any initial physical …
composing augmented dynamic that guaranteed to be able to regulate any initial physical …
[PDF][PDF] Quaternion-based Attitude Control Systems Design of Single Spacecraft and Cooperative Spacecrafts: Boundedness Solution Approach
It is well-known that single equilibrium orientation point in matrix rotation is represented by
two equilibrium points in quaternion. This fact would imply to nonefficient control effort as …
two equilibrium points in quaternion. This fact would imply to nonefficient control effort as …