Contents: Hybrid guidance and navigation systems; Characteristics of a satellite navigation system operated in conjunction with a user inertial system; Global navigation/traffic surveillance/communication satellite system for military and civil vehicles; The TMA role of hybrid system radio sensors; The use of filtering techniques and/or 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 VOR/DME; Optimal correction of stochastic errors of inertial systems; Design of low sensitivity Kalman filters for hybrid navigation systems.


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    Title :

    Hybrid Navigation Systems


    Contributors:

    Publication date :

    1970


    Size :

    320 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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