When the UAV goes to high altitudes such that the observed surface of the earth becomes planar, the structure and motion recovery of the earth\u27s moving plane becomes ambiguous. This planar degeneracy has been pointed out very often in the literature; therefore, current navigation methods either completely fail or give many confusing solutions in such scenario. Interestingly, the horizon line in planar scenes is straight and distinctive; hence, easily detected. Therefore, we show in this paper that the horizon line provides two degrees of freedom that control the relative orientation between the camera coordinate system and the local surface of earth. The recovered degrees of freedom help linearize and disambiguate the planar flow, and th...
The utility of the horizon for airborne sense-and-avoid (ABSAA) applications is explored in this wor...
The utility of the horizon for airborne sense-and-avoid (ABSAA) applications is explored in this wor...
We develop a method for estimating the flight critical parameters of pitch angle, roll angle and the...
When the UAV goes to high altitudes such that the observed surface of the earth becomes planar, the ...
Abstract — A critical step in navigation of unmanned aerial vehicles is the detection of the horizon...
Abstract — A critical step in navigation of unmanned aerial vehicles is the detection of the horizon...
Attitude (pitch and roll angle) estimation from visual information is necessary for GPS-free navigat...
Attitude (pitch and roll angle) estimation from visual information is necessary for GPS-free navigat...
Attitude (pitch and roll angle) estimation from visual information is necessary for GPS-free navigat...
The last decade has seen a dramatic expansion in the deployment of Unmanned Airborne Vehicles (UAVs)...
Planetary rovers navigate in extreme environments for which a Global Positioning System (GPS) is una...
International audienceAttitude (roll and pitch) is an essential data for the navigation of a UAV. Ra...
International audienceUnmanned Aerial Vehicles (UAVs) are the subject of an increasing interest in m...
International audienceAttitude is one of the most important parameters for a UAV during a flight. At...
The paper describes how the attitude of a sounding rocket, launch vehicle or satellite with respect ...
The utility of the horizon for airborne sense-and-avoid (ABSAA) applications is explored in this wor...
The utility of the horizon for airborne sense-and-avoid (ABSAA) applications is explored in this wor...
We develop a method for estimating the flight critical parameters of pitch angle, roll angle and the...
When the UAV goes to high altitudes such that the observed surface of the earth becomes planar, the ...
Abstract — A critical step in navigation of unmanned aerial vehicles is the detection of the horizon...
Abstract — A critical step in navigation of unmanned aerial vehicles is the detection of the horizon...
Attitude (pitch and roll angle) estimation from visual information is necessary for GPS-free navigat...
Attitude (pitch and roll angle) estimation from visual information is necessary for GPS-free navigat...
Attitude (pitch and roll angle) estimation from visual information is necessary for GPS-free navigat...
The last decade has seen a dramatic expansion in the deployment of Unmanned Airborne Vehicles (UAVs)...
Planetary rovers navigate in extreme environments for which a Global Positioning System (GPS) is una...
International audienceAttitude (roll and pitch) is an essential data for the navigation of a UAV. Ra...
International audienceUnmanned Aerial Vehicles (UAVs) are the subject of an increasing interest in m...
International audienceAttitude is one of the most important parameters for a UAV during a flight. At...
The paper describes how the attitude of a sounding rocket, launch vehicle or satellite with respect ...
The utility of the horizon for airborne sense-and-avoid (ABSAA) applications is explored in this wor...
The utility of the horizon for airborne sense-and-avoid (ABSAA) applications is explored in this wor...
We develop a method for estimating the flight critical parameters of pitch angle, roll angle and the...