PPT-Inertial Navigation System (INS)

Introduction to INS INS is a navigation aid that uses a computer motion sensors and rotation sensors The motion sensors such as accelerometers The rotational sensors such as gyroscopes. Kottas and Stergios I Roumeliotis Department of Computer Science and Engineering University of Minnesota Minneapolis MN dkottas stergios at csumnedu Abstract This paper addresses the problem of visualinertial navigation when processing camera observ Slotine Nonlinear Systems Laboratory Massachusetts Institute of Technology Cambridge Massachusetts 02139 USA yongzhaomitedu jjsmitedu Abstract We derive an exact deterministic nonlinear observer to compute the continuous state of an inertial navigat Always relative to inertial space Most common inertial sensors Accelerometers G yros brPage 4br Accelerometers By attaching a mass to a spring measuring its deflection we get a simple accelerometer Figure Gade 2004 brPage 5br Accelerometers conti Hesch Dimitrios G Kottas Sean L Bowman and Stergios I Roumeliotis joel dkottas bowman stergios csumnedu Department of Computer Science Engineering University of Minnesota Multiple Autonomous Robotic Systems Labroratory Technical Report Number 20120 Navigation . Sensors and INS Mechanization. Tuesday 12 Feb 2013. NMT EE 570: Location and Navigation: Theory & Practice. Slide . 1. of 19. Navigation Sensors and INS . Mechanization . Inertial Sensors. Tuesday 15 Jan 2013. NMT EE 570: Location and Navigation: Theory & Practice. Slide . 1. of . 17. Course Outline. Tuesday 15 Jan 2013. NMT EE 570: Location and Navigation: Theory & Practice. Slide . Michael Bekkala. Michael Blair. Michael Carpenter. Matthew Guibord. Abhinav Parvataneni. Dr. Shanker Balasubramaniam. Background. Accessibility. Popularity of GPS and INS. Cell phones. Apple iPhone, Blackberry, Android platform. Navigation . Sensors and INS Mechanization. Tuesday 26 Feb 2013. NMT EE 570: Location and Navigation: Theory & Practice. Slide . 1. of 14. Navigation Sensors and INS Mechanization . Navigation . Kyle . Corkey. Devan. Corona. Grant Davis. Nathaniel . Keyek-Franssen. Robert Lacy. John . Schenderlein. Rowan . Sloss. Dalton Smith. Customer. Dr. Suzanna. . Diener. -. Northrop. Grumman. Faculty Advisor. “GUIDANCE SYSTEMS”. By,. Vivek S. Mutgekar. USN:2GI07ME113. B-14. Introduction:. A cruise missile is basically a small, . pilotless airplane. . Cruise missiles have an 8.5-foot (2.61-meter) wingspan, are powered by turbofan engines and can fly 500 to 1,000 miles (805 to 1,610 km) depending on the configuration. A cruise missile's job in life is to deliver a 1,000-pound (450-kg) high-explosive bomb to a precise location -- the target. Micro-Technology forPositioning, Navigation and Timing(µPNT) Dr. Andrei M. Shkel Program Manager DARPA/MTO Approved for Public Release, Distribution Unlimited Andrei M. Shkel Aggregation Overall goal One or more of the Following Statements may affect this DocumentThis document has been reproduced from the best copy furnished by the organizationalsource It is being released in the interest of makin Certain functions of . E. and . H. are invariant under Lorentz transform. The 4D representation of the field is . F. ik. F. ik. . F. ik. = an invariant scalar. (1/2). e. iklm. . F. ik. . F. lm. Inertial navigation is widely used for the guidance of aircraft, ships, missiles and vehicles. This introduction to the system covers basic principles, system mechanics, instrumentation, computation and design analysis. The text features a particularly contemporary treatment of inertial sensors and computational techniques for error analysis. It also describes integrated systems incorporating additional navigational aids and examples of current applications in both civilian and military situations.