The Navigation Potential of Ground Feature Tracking

Abstract

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 method of least square. Concerning the second step: checking observability for the 3-D case shows that at least 2 objects need to be tracked. In practice one needs to track more than two objects to wash out the measurement error and obtain good results.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 2009
Accession Number
ADA506512

Entities

People

  • Guener Mutlu

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Autonomy
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Algorithms
  • Collision Avoidance
  • Coordinate Systems
  • Department Of Defense
  • Detection
  • Geometry
  • Global Positioning Systems
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Measurement
  • Micro Air Vehicles
  • Navigation
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Engineering

Readers

  • Control Systems Engineering.
  • Inertial Navigation Systems.
  • Sensor Fusion and Tracking Systems.

Technology Areas

  • Space
  • Space - Space Objects