Inertial navigation system algorithm block diagram. Taken from Titterton & Weston (2004) The navigation equations presented in the image above is collectively known as the INS (Inertial Navigation System). The output of INS consists of the complete system position, velocity, acceleration, orientation and angular rates of rotation. These parameters are used by the control system as the measurements of the system motion on which the control action will be performed.
Linked | INS take Gravity, Earth Rotation and Coriolis into account |
Image Url | www.researchgate.net |
From Doc | ![]() |
Source | www.researchgate.net |
Authors | Johan Meyer, Francois du Plessis, WA Clarke |
Published | January 2009 |
Upload | Saturday, August 13, 2022; wabis |
Size | 65.2 kB |
Scale | 702 x 433 Pixel |