A real-time six-degree-of-freedom hybrid simulation facility for guidance system testing

1973 ◽  
Author(s):  
J. HOGAN ◽  
J. WELCH
2018 ◽  
Vol 84 (867) ◽  
pp. 18-00229-18-00229
Author(s):  
Shigeyuki KOBAYASHI ◽  
Yoshitaka YAMASHITA ◽  
Takayuki USUDA ◽  
David P. STOTEN

2005 ◽  
Vol 2 (1) ◽  
pp. 155-165
Author(s):  
Baghdad Science Journal

Many of accurate inertial guided missilc systems need to use more complex mathematical calculations and require a high speed processing to ensure the real-time opreation. This will give rise to the need of developing an effcint


2021 ◽  
Author(s):  
Ningning Shi ◽  
Shengtong Wang ◽  
Gaopeng Xue ◽  
Mengfang Liu ◽  
Yaodong Han ◽  
...  

Author(s):  
Alexander Yuen ◽  
Yusuf Altintas

This paper presents a methodology to compensate the tooltip position errors caused by the geometric errors of a three-axis gantry type micromill integrated with a six degree-of-freedom (6DOF) rotary magnetic table. A geometric error-free ideal forward kinematic model of the nine-axis machine has been developed using homogenous transformation matrices (HTMs). The geometric errors of each linear axis, which include one positioning, two straightness, pitch, roll, and yaw errors, are measured with a laser interferometer and fit to quintic polynomial functions in the working volume of the machine. The forward kinematic model is modified to include the geometric errors which, when subtracted from the ideal kinematic model, gives the deviation between the desired tooltip position with and without geometric errors. The position commands of the six degree-of-freedom rotary magnetic table are modified in real time to compensate for the tooltip deviation using a gradient descent algorithm. The algorithm is simulated and verified experimentally on the nine-axis micromill controlled by an in-house developed virtual/real-time open computer numerical controlled (CNC) system.


Sign in / Sign up

Export Citation Format

Share Document