Accession Number:

AD0701775

Title:

HYBRID NAVIGATION SYSTEMS.

Descriptive Note:

Conference proceedings,

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1970-01-01

Pagination or Media Count:

320.0

Abstract:

Contents Hybrid guidance and navigation systems Characteristics of a satellite navigation system operated in conjunction with a user inertial system Global navigationtraffic surveillancecommunication satellite system for military and civil vehicles The TMA role of hybrid system radio sensors The use of filtering techniques andor mixed navigation systems in combination with barometric altimetry to generate glide slopes for precision approach The use of inertial information to improve automatic ILS approach performance Improvement of the accuracy of automatic landing systems by use of Kalman-filtering techniques and incorporation of inertial data Collision avoidance and the air traffic control environment Integrated hybrid-inertial aircraft navigation systems Modern aircraft navigation sensors for hybrid systems Loran systems technology Systeme de navigation a inertie hybride optimise Tactical loran The C-5 navigation system - an application of digital synergistic stochastic hybrid navigation technology The hybrid navigation system for the nimrod maritime patrol aircraft The use of hybrid techniques in commercial transport aircraft Integrated avionic system design for helicopters and VTOL Integrated navigation by least square adjustment A simple Kalman filter for VORDME Optimal correction of stochastic errors of inertial systems Design of low sensitivity Kalman filters for hybrid navigation systems.

Descriptors:

Subject Categories:

  • Air Navigation and Guidance

Distribution Statement:

APPROVED FOR PUBLIC RELEASE


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