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G. M. Soloviov, J. G. Krimova.
THEORY ORBITS OF STATIONARY HEIGHTS
Class of orbits stationary heights (ОSH) is determined, as a plethora orbits of an artificial Earth satellites into non-central gravitational field. Heights its orbits in each point up of not changes during of time. Basic properties of these orbits are given. Formulas for account parameters of orbits with given characteristics and formulas for account instantaneous orbits parameters are given. In Appendix basic formulas for account periodic perturba-tions parameters of orbits stationary heights in non-central gravitational field are given.
V. S. Chaplinskiy, I. I. Makhnenko.
METHODS AND TYPICAL TECHNOLOGY OF NAVIGATING MEASUREMENTS IN A GROUND-SPACE COMMAND-INFORMATION NETWORK
Elements of theory, methods and initial technologies of navigating measurements in units ground-space com-mand-retranslation network are resulted. requirements to stability frequency of driving generators, to checking local time scales of units network, to accuracy apriory information on movement units are estimated. Analyzed achievable accuracy trajectory of control space vehicles.
M. V. Levskiy
PERFECTING OF MOTION CONTROL SYSTEMS AND NAVIGATING ON PATH CREATION OF OPTIMAL CONTROL ALGORITHMS
Milestones of development and perfecting of motion control systems spacecraft are briefly described. Then, principles of construction and capability of modern automatic systems mission control are reviewed. Presence digital control system allows to apply most perfect algorithms and any control laws practically. Is rotined, that leading particular modern control systems is software. Namely new, more perfect onboard software determines paths and level of development autonomous control systems. On example of rocket "Energia" is demonstrated, that presence of algorithms of onboard processing command devices measurements allows to refuse installation padding sensors overloads on body of rocket. As other example, solution problem of optimization spatial reorientation of weighty spacecraft has served.
I. I. Makhnenko, V. I. Prut, V. S. Chaplinskiy.
APPLICATION ACCOMPANYING RETRANSLATION OF MEASUREMENTS FOR CONTROL ORBITS OF DEDUCING SPACE VEHICLES
Application technologies trajectory of control deducing orbits of rocket space purpose "Proton "- M" - amaining block ""Briz-M" of paying loads into geotransitive and geostationary orbits with using retranslation measurements allows to define actual parameters of movement orbital block with accuracy, sufficient for without searching entry in communication with orbital block by means of ground measuring complex.
V. P. Konovalov, V. P. Gerastovskiy, V. I. Prut.
QUESTIONS OF GLOBAL TELEMETRIC CONTROL FLIGHT ROCKETS OF SPACE PURPOSE
Basic ways of perfection information-telemetric maintenance start RKN on non-equipped lines are creation unified small-mass mobile telemetric measuring items, perspective multifunctional space system relaying various kinds of information from objects RKT, and also edge of hardware-software means compression telemetric information.
M. A. Astrakhancev, A. N. Dubovoi, D. S. Kolev, V. P. Plotnimov, A. P. Romanenko, M. P. Simonov, A. A. Chuiko.
PROBLEMS AND METHODICAL CIRCUITS OF SUBSTANTIATION SHAPE PERSPECTIVE SYSTEM OF SPACE MEANS ARMS.
Methodical circuits of formation offers in project basic directions works on a space weapons system, realization researches by definition tactic-technical and economic shape of space complex are resulted
M. A. Astrakhancev, A. N. Dubovoi, D. S. Kolev, V. P. Plotnimov, A. P. Romanenko, M. P. Simonov, A. A. Chuiko.
CRITERION AND PARAMETERS OF EFFICIENCY OPERATION KCV
It is offered as global forecasting criterion at an estimation alternatives perspective system space arms to accept target efficiency of perspective system. Some questions of perfection methodology complex substantiation of rational variant of system KSV, estimation of efficiency, structure criteria device and choice system parameters for an estimation efficiency of chosen variant system are set up.
M. A. Astrakhancev, A. N. Dubovoi, D. S. Kolev, V. P. Plotnimov, A. P. Romanenko, M. P. Simonov, A. A. Chuiko.
BASES OF PROGRAMMING DEVELOPMENT SPACE MEANS OF ARMS: FORMATION STATE PROGRAMS OF ARMS AND STATE DEFENСЕ ORDER ON SPACE MEANS. STRUCTURE AND STRUCTURE OF TECHNIQUES
Some features of models and techniques used at substantiation prospects for development of space complexes and systems of information maintenance of actions Armed forces of Russian Federation are considered.
A. N. Dubovoi, A. P. Romanenko.
METHODS OF SUBSTANTIATION PROSPECTS FOR DEVELOPMENT OF SPACE MEANS
In given clause have received further development approaches to consideration and classification methods of substantiation prospects for development space means which have been set up to authors in a series of publications 2000-2001. In particular, methods of system analysis connected to application theory of sets, and also structurally functional approach.
A. N. Dubovoi
PROBLEMS OF DEVELOPMENT OF SPACE MEANS
The general circuit researches of tactic-characteristics and principles research systems of space arms is given.
L. A. Pchelincev, I. I. Kuznecov, L. I. Slabkiy
ESTIMATIONS OF DEFORMATION CASUAL CONSTRUCTIONAL FIELDS
In clause casual deformation of design space flying device a proxyed by some trellised casual field. Given at expansion considered site of design top and bottom estimations for general casual deformation of given site. Ideology of central limiting theorem theory of probabilities is used.
L. A. Pchelincev, I. I. Kuznecov, A.S. Ershov.
MIXED POISSON PROCESSES AND THEIR APPLICATION IN INSURANCE SPACE IS BRAVE
In clause generalization mathematical model process of insurance space will be carried out brave on a case when dot process of moments time of realization insurance events is not simply poisson process, and mixed poisson by process. Approximation for probability of ruin abandonee also is given
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