This research effort examines the reduction of error in inertial navigation aided by vision. This is part of an effort focused on navigation in a GPS denied environment. The navigation concept examined here consists of two main steps. First, extract the position of a tracked ground object using vision and geo-locate it in 3 dimensional navigation frame. In this first step multiple positions of the UAV are assumed known; think of a synthetic aperture. The only information about the tracked ground objects/features is the unit vector that points to the objects from the center of the camera. Two such vectors give enough information to calculate the best estimate of the position of the tracked object in a 3 dimensional navigation frame using the...
Navigation performance in small unmanned aerial vehicles (UAVs) is adversely affected by limitations...
A method human operated INS aiding is explored in which the pilot identifies and tracks a ground fea...
Traditionally, the task of determining aircraft position and attitude for automatic control has been...
AFIT/GE/ENG/09-52 This research effort examines the reduction of error in inertial navigation aided ...
The reduction of the navigation error in an inertial navigation system by optically tracking a groun...
The motivation of this research is to address the use of bearing-only measurements taken by an optic...
Navigation systems of unmanned aircraft systems (UAS) are heavily dependent on the availability of G...
Inertial Navigation System (INS) aiding using bearing measurements taken over time of stationary gro...
Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.DOI: 10.2...
This paper demonstrates the use of Global Positioning System (GPS) and Inertial Navigation System (I...
The need addressed in this thesis is to provide an Autonomous Ground Vehicle (AGV) with accurate inf...
Unmanned vehicles are increasingly common in our world today. Self-driving ground vehicles and unman...
Ph. D. Thesis.Unmanned aerial vehicles (UAVs) are now well-established as platforms for photogrammet...
Published in the Journal of Aerospace Computing, Information, and Communication, Vol. 2, September 2...
There has been increasing interest in developing the ability for small unmanned aerial systems (SUAS...
Navigation performance in small unmanned aerial vehicles (UAVs) is adversely affected by limitations...
A method human operated INS aiding is explored in which the pilot identifies and tracks a ground fea...
Traditionally, the task of determining aircraft position and attitude for automatic control has been...
AFIT/GE/ENG/09-52 This research effort examines the reduction of error in inertial navigation aided ...
The reduction of the navigation error in an inertial navigation system by optically tracking a groun...
The motivation of this research is to address the use of bearing-only measurements taken by an optic...
Navigation systems of unmanned aircraft systems (UAS) are heavily dependent on the availability of G...
Inertial Navigation System (INS) aiding using bearing measurements taken over time of stationary gro...
Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.DOI: 10.2...
This paper demonstrates the use of Global Positioning System (GPS) and Inertial Navigation System (I...
The need addressed in this thesis is to provide an Autonomous Ground Vehicle (AGV) with accurate inf...
Unmanned vehicles are increasingly common in our world today. Self-driving ground vehicles and unman...
Ph. D. Thesis.Unmanned aerial vehicles (UAVs) are now well-established as platforms for photogrammet...
Published in the Journal of Aerospace Computing, Information, and Communication, Vol. 2, September 2...
There has been increasing interest in developing the ability for small unmanned aerial systems (SUAS...
Navigation performance in small unmanned aerial vehicles (UAVs) is adversely affected by limitations...
A method human operated INS aiding is explored in which the pilot identifies and tracks a ground fea...
Traditionally, the task of determining aircraft position and attitude for automatic control has been...