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.
Hybrid Navigation Systems
1970
320 pages
Report
No indication
English
NTIS | 1989
|NTIS | 1987
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