Journal "Gyroscopy and Navigation" /  Books  
   "Gyroscopy and Navigation" №4, 2008


N.V. Mikhailov, V.F. Mikhailov An ambiguity resolution method for the GPS phase measurements at the spaceship relative navigation 9
Considered is the method of ambiguity resolution for satellite-based GPS phase measurements, which takes into account the specific character of the problem of spacecraft relative navigation. This method provides for obtaining a fixed and a floating solution. Distinction of the proposed fixed solution consists in its layout into two stages and in more efficient arrangement of the integer search of phase measurement periods. At the first stage of the fixed solution the most probable value of the phase period integer is retrieved. At that, the exhaustive search of the period integer is not performed. High speed of this stage implementation is provided by the fact that the domain, in which searching is executed, is being continuously narrowed as far as new "candidates" for a more probable value are found. The second stage serves for estimating a posterior probability of a determined value of the period integer. It is essential that the estimation of a posterior probability is formed step-by step in the course of exhausting searching for possible values of the period integer. Moreover, the value of an estimate of posterior probability monotonely decreases while new integer values are being registered. Owing to such a method it becomes possible to abandon an uncertain fixed solution without complete calculation of its posterior probability and exhaustive search of all possible phase period values.
Gerd Boedecker Precision aircraft attitude determination with multi-antennae GPS receivers 21
A.Ye. Pelevin Parameter identification for a model of marine vehicle at the active control periodic motion 29
The method for a vehicle model parameters identification under active control providing for its motion periodic nature has been proposed. It has been shown that using the vehicle motion features some additional equations can be obtained that connect the parameters being identified. These equations can be effectively used when estimating the model parameters under external disturbances condition. The application of this approach to the parameters identification of a survey vessel model has been presented.
I.Ye. Gutner, L.D. Zhuravlev, Ye.N. Zvorykin, A.A. Molochnikov, M.V. Orlov Calculation of the current glide slope angle for the aircraft landing on the aircraft-carrier deck 40
Using spherical trigonometry method, the equation was obtained which describes the law of generation of the aircraft commanded glide slope α(=ILU) (materialized as a green ray of indicating light) relative to the rocking aircraft-carrier deck. A block diagram of algorithm for generation of the stated angle is worked out. This angle provides stabilization of the prescribed glide slope α(=GS) relative to the deck averaged position with account for the aircraft-carrier static angles of trim and roll. Then the commanded glide slope α and hook-to-eye distance compensation angle of the aircraft are smoothly followed according to cosine law. The use of the obtained law of generating the current angle α commanded to stabilization drive increases the glide slope stabilization accuracy, decreases deflection of the aircraft hook to aircraft-carrier deck touchdown point from the designed one and, therefore, increases safety of the aircraft landing upon the aircraft-carrier.
I.A. Terentyev Functional diagnosis and testing of a gimbal inertial navigation system servosystem 49
The paper presents the basic concept and results of INS servo system diagnostic system development. The diagnostic system consists of functional and test parts which are realized in all of modes of operation. The functional diagnostic in gyroscopic stabilization mode is based on instrument control of dynamic misalignment and informational control of INS invariant behavior - cosine angle of ESG angular momentums. The test control corresponds control of shift velocity tryout in servo system command channel. The concept of two-level informational control is justified. Such informational control must show instrumental failures and informational abnormalities in INS operation.
D.O. Taranovsky Bench calibration of pendulous floated accelerometers of a shipborne inertial navigation system 56
The results of development of a pendulum pulse-rebalance accelerometer unit (AU) calibration procedure is presented. For AU used on mobile objects with a smaller acceleration range, development of a procedure for calibration in the AU operating range of angles is relevant.
For calibration the AU is mounted on a single-axis turn-table which provides the possibility for the AU to be fixed in two opposite positions at an angle of 45o relative to the axis of rotation.
The distinctive features of the proposed calibration technique are as follows:
  • calibration is performed in the operating range of acceleration for exclude the errors due to the AU model inadequacy. That is typical for the pulse-rebalance accelerometer when calibrated in the range of ±g,
  • the parameters are evaluated jointly with the AU installation errors using the statistical estimation methods to smooth over the measurement errors,
  • an iterative procedure is used to exclude the model inadequacy in the case of large installation errors.
AU interchangeability assurance method for gimbal inertial navigation system is considered. The experimental results presented provide support for the efficiency of the proposed calibration technique.
2nd Russian Multiconference on Control Problems (2RMCCP-2008) 66

26th Conference in memory of N.N.Ostryakov
Abstracts of the papers
Session Gyro Sensors of Navigation and Control Systems

S.F. Konovalov, J.B.Seo Magnetic field distribution in the annular gap of a torque sensor of a Q-flex type accelerometer 67
V.Ya. Raspopov, D.M. Malyutin, R.V. Alaluev, Yu.V. Ivanov Accelerometer of increased accuracy for an unmanned aerial vehicle -
V.E. Dzhashitov, V.M. Pankratov, A.V. Golikov Computer research and educational lecture courses in the engineering mechanics, general and applied theory of gyros 68
M.A. Barulina, V.E. Dzhashitov, V.M. Pankratov Increasing micromechanical accelerometer accuracy by means of using reversible thermal control system on Peltier coolers 70
A.I. Panferov, V.K. Ponomarev, L.A. Severov, N.A. Ovchinnikova Estimation of micromechanical gyroscope parameters 71
L.A. Severov, Ye.V. Ivanova, A.A. Tyrtychny Kinematics and dynamics of micromechanical gyroscope based on ring resonator -
D.V. Rozentsvein Applied shock influence on micromechanical gyroscope operation       -
A.S. Kovalev, Ye.V. Logovskaya Analysis of micromechanical gyroscope errors when operating on a high-dynamic vehicle 73
S.G. Romanenko, S.L.Levin, T.V. Panich Precessional motion of electrostatic gyroscope rotor under space conditions 74
S.N. Belyaev, A.G. Scherbak Investigation of process of a hyperfine film coating thermal spraying on spherical knots of gyrodevices -
G.I. Yemelyantsev, B.Ye. Landau, S.L. Levin, B.V. Odintsov, S.G. Romanenko Increasing accuracy of a strapdown attitude reference system on electrostatic gyroscopes with the use of automatic specification of the drift model factors during space operation -
A.P. Buravlev, V.M. Kuzin, B.Ye. Landau, V.V. Sumarokov Gimballess electrostatic double electrode suspension gyroscope 75
V.I. Zavgorodny, B.V. Odintsov Influence of electromagnetic fields on the parameters of a gimballess electrostatic solid rotor gyroscope -
Gyroscope drive control under starting conditions       76
S.A. Vasyukov, G.F. Drobyshev Simulation of impact electrostatic suspensions -

Session Gyroscopic and Integrated Inertial Satellite Systems

M.V. Konash, V.P. Golikov, A.A. Golovan, N.B. Vavilova Integration algorithm for the SINS on micromechanical sensors with SNS according to the restart pattern 77
L.P. Nesenyuk, D.V. Volynsky, B.A. Blazhnov, G.I. Yemelyantsev, A.P. Stepanov, I.V. Semenov, D.A. Radchenko, D.I. Lychev Integrated inertial satellite attitude and navigation system with a micromechanical inertial unit. Results of testing on a motor vehicle -
A.M. Boronakhin, L.N. Oleinik, N.S. Filipenya Small-sized integrated rail track fault detection system 78
Ye. I. Somov Design and flight calibration of the astroinertial spacecraft sensing system -
V.Z. Gusinsky, Yu. A. Litmanovich, I.A. Terentyev Information check in the diagnostic system for the shipborne INS on uncontrolled gyros 79
Yu. A. Litmanovich, A.A. Stolbov One method of error model linearization for the INS on uncontrolled gyros 80
S.A. Chernikov, Li Ming Damping of gyro system resonance oscillations by the active feedback dynamic damper -
A.V. Polushkin, L.Ya. Kalihman, D.M. Kalihman, S.F. Nahov, R.V. Yermakov, D.A. Belyakov, S.N. Shatskov, V.A. Lomov, A.D. Shapran A general-purpose hardware for the computer check of a wide class of inertial devices: development results -
V. Yu. Lapin, V.S. Lobanov, V.N. Zboroshenko, N.V. Tarasenko Development of a scaled-down table simulator for investigation and execution of algorithms for attitude and stabilization systems of future-technology spacecrafts 82

Session Navigation Data Processing and Motion Control

A.I. Naumov, V.A. Merkulov Informativity analysis procedure for models of the terrain height field in the correlation-extreme navigation problem 82
S.A.Kosyachenko, A.I. Naumov Sequential search algorithm of the correlation-extreme navigation at estimation of coordinate and velocity errors 83
S.M. Yelsakov, V.I.Shiryaev Provision of accuracy in determination of unmanned aircraft coordinates at landing 84
O.A. Stepanov, A.B. Toropov Comparison of suboptimal linear algorithms with the optimal algorithm in nonlinear navigation problems -
Yu.P. Ivanov, L.S. Krashenko Algorithm of spectral-Markov nonlinear filtering of navigation signals 85
V.A. Vasilyev, O.A. Stepanov, A.V. Osipov Application of fuzzy logic when solving nonlinear navigation estimation tasks 86
A.V.Chernodarov, A.I.Shigin Checkup and state estimate of strapdown inertial navigation systems by reliability level -
G.V. Bezmen, N.V. Kolesov Functional diagnosis of dynamic systems with the use of a fuzzy technical state model 87
S.B. Berkovich, N.I. Kotov, A.V. Sholokhov, R.N. Sadekov, V.A. Liventsev Estimation of precision factors of the integrated autonomous terrain navigation systems in view of possible errors in the external correction information -
Yu.P.Ivanov, A.N.Zhuravlev Study of the spectral method of reliability estimation of an airborne vehicle flight safety 88
Ye.V. Shevtsova Application of the theory of bursts in the navigation data processing tasks 89
K.Ye. Afanasyeva, V.I. Shiryaev Guaranteed estimation by the information on the group of entities 89
M.V.Drozdov Identification of influences and diagnostics of a spacecraft state by the signals of accelerometers as microacceleration meters 91
N.N. Scheglova Diagnostics of unsafe sections at monitoring of long-length structures -
M.B.Rozengauz Operation correctness estimation for algorithms and systems with the use of fuzzy measure 92
Yu.P.Ivanov, V.G.Nikitin, M.V.Fomin The integrity estimation method for a satellite navigation system in view of the equipment reliability 93
M.B. Bogdanov, A.V. Prokhortsov, V.V. Savelyev, V.A. Smirnov, A.A. Chepurin The method of increasing accuracy of the navigation problem solution in satellite radio navigation systems -
V.M. Nikiforov Synthesis problems of terminal regulators for dynamic system motion control with consideration for pure time delay 95
V.G. Borisov, G.N. Nachinkina, B.V.Pavlov, A.M. Shevchenko New algorithmic aids and software for designing aircraft flight control systems 96
A.V. Pesterev, L.B. Rapoport Invariant set estimation in the stabilization problem of the wheeled robot motion along a curved path 97
A.V.Timofeev, O.A. Derin Three-dimensional sensor on the basis of stereoscopic vision and laser rangefinder 98
A.V. Nebylov, V.A. Nebylov The current anisotropy analysis of the disturbed sea surface for the hydroplane landing mode optimization -
A.I. Grekov, Yu.P. Ivanov, A.V. Loparev, A.V. Nebylov Prediction of the vessel guide screw baring moments at heavy sea 99
S.A. Brodsky, A.V. Nebylov, A.I. Panferov Optimization of the sensor systems for elastic vehicles and structures control 100
A.N.Mikryukov, A.I. Naumov Algorithmic provision for integration of the strapdown inertial and relief-metric correlation-extreme navigation systems -
A.V. Grinenkov, T.A. Silina Integration algorithms for the information incoming from the outputs of heterogeneous undersea observation channels 101

Session Electronics and Computer Engineering of Onboard Systems

V.A. Zimin, N.A. Lookin History of development of the onboard computer engineering for the rocket and space complexes developed at Science and Production Association of Automatics 102
S.G. Bobkov Advanced computer systems based on RapidIO standard -
I.V.Karabanov, M.A. Linnik The high-precision module of hydroacoustic navigation system for slant range determination 103
N.A.Lookin Optimum architectures of onboard function-specific processors for correlation-extreme navigation systems of highly-maneuverable flying vehicles 104
A.V. Nebylov, A.V. Samokish, K.D. Smolin, P.A. Sumbarov Formal language for designing onboard computer systems 105
S.V. Kalin, V.I. Klepikov, Yu.N.Dudorov, D.S.Podkhvatilin Basic information technology of the integrated modular control systems 106
V.V. Balashov, A.G. Bakhmurov, D.Yu. Volkanov, R.L. Smelyansky, M.V. Chistolinov, N.V. Yuschenko, G.T. Mamontov, P.V. Yukhta Experience of software environment DIANA application to simulation and integration of onboard computer systems 107
A.N. Godunov, P.Ye. Nazarov, I.I. Khomenkov Operating real-time system ORTS Baget 3.0 108
Yu.N.Dudorov, V.I. Klepikov, V.S. Strizhevsky Functionality of the certifiable software development environment 109
A.N. Godunov, A.I. Gryuntal The real-time software of Baget computer family 110
S.V. Kalin, V.I. Klepikov, Yu.N.Dudorov, D.S.Podkhvatilin Analytic redundancy in distributed control systems -
N.V. Kolesov, A.A. Sokolov, M.V. Tolmacheva Diagnostics tools design principles for real-time systems 111
O.K. Yepifanov, M.V. Orlov Nonlinearity compensation of the mechanical characteristic of multipolar erection torque motors being part of gearless follow-up motor 112

International Public Association
The Academy of Navigation and Motion Control
Official information

The 26th General Meeting of the Academy of Navigation and Motion Control 113
L.N. Shalimov, S.F. Deryugin, L.N. Belsky Academician N.A. Semikhatov and his role in designing rocket and space technology and in developing applied science. To the 90th birth anniversary (1918 - 2002) 116

New books

About D.M. Kalihman's book "Precision controllable test benches for dynamic tests of gyroscopic devices" 119


Russian and international conferences, symposia and exhibitions 121
Centrifuges as the main means for setting a constant linear acceleration in the range above 1 g 125
Abstracts of the published papers 127
List of the materials published in the journal Gyroscopy and Navigation in 2008 130

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Last updated December 30, 2008.