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  • 1
    Publication Date: 2019-06-27
    Description: Algorithms for failure detection, isolation, and correction of redundant inertial instruments in the strapdown dodecahedron configuration are competitively evaluated in a digital computer simulation that subjects them to identical environments. Their performance is compared in terms of orientation and inertial velocity errors and in terms of missed and false alarms. The algorithms appear in the simulation program in modular form, so that they may be readily extracted for use elsewhere. The simulation program and its inputs and outputs are described. The algorithms, along with an eight algorithm that was not simulated, also compared analytically to show the relationships among them.
    Keywords: NAVIGATION
    Type: NASA-CR-124234 , TRW-18313-6004-RU-00
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: Seven algorithms for failure detection, isolation, and correction of strapdown inertial instruments in the dodecahedron configuration are competitively evaluated by means of a digital computer simulation that provides them with identical inputs. Their performance is compared in terms of orientation errors and computer burden. The analytical foundations of the algorithms are presented. The features that are found to contribute to superior performance are use of a definite logical structure, elimination of interaction between failures, different thresholds for first and second failures, use of the 'parity' test signals, and avoidance of iteration loops.
    Keywords: NAVIGATION
    Type: AIAA PAPER 73-853 , Guidance and Control Conference; Aug 20, 1973 - Aug 22, 1973; Key Biscayne, FL
    Format: text
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  • 3
    Publication Date: 2019-07-13
    Description: Strapdown redundant experimental sensor inertial navigation package containing gyros and accelerometers, discussing signal real time processing by digital computer
    Keywords: NAVIGATION
    Type: AIAA PAPER 69-851 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, GUIDANCE, CONTROL, AND FLIGHT MECHANICS CONFERENCE; Aug 18, 1969 - Aug 20, 1969; PRINCETON, NJ|; ADEMIE DES SCIENCES
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  • 4
    Publication Date: 2019-07-13
    Description: Strapdown redundant experimental sensor inertial navigation package containing gyros and accelerometers, discussing signal real time processing by digital computer
    Keywords: NAVIGATION
    Type: AIAA PAPER 69-851 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, GUIDANCE, CONTROL, AND FLIGHT MECHANICS CONFERENCE; Aug 18, 1969 - Aug 20, 1969; PRINCETON, NJ
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