TRACKING OF PHOBOS-GRUNT MISSION IN LOW EARTH ORBIT Alexander S. Samotokhin, Andrey G. Tuchin M.V. Keldysh Institute of Applied Mathematics of Russian.

Slides:

Advertisements

Similar presentations

The ballistic support of the “SPECTR-RG” spacecraft flight to the L2 point of the Sun-Earth system I.S. Ilin, G.S. Zaslavskiy, S.M. Lavrenov, V.V. Sazonov,

Advertisements

ARO309 - Astronautics and Spacecraft Design Winter 2014 Try Lam CalPoly Pomona Aerospace Engineering.

MAE 4262: ROCKETS AND MISSION ANALYSIS Orbital Mechanics and Hohmann Transfer Orbit Summary Mechanical and Aerospace Engineering Department Florida Institute.

Golubev Yu.F., Grushevskii A.V., Koryanov V.V., Tuchin A.G. A method of orbits designing using gravity assist maneuvers to the landing.

Институт прикладной математики им. М.В.Келдыша РАН Keldysh Institute of Applied Mathematics, Russian Academy of Sciences.

ECE 5233 Satellite Communications

Possible Orbits for the First Russian/Brazilian Space Mission Alexander A. Sukhanov Space Research Institute (IKI) of Russian Academy of Sciences Moscow,

Guaranteed Approach For Orbit Determination With Limited Error Measurements Zakhary N. Khutorovsky Interstate Joint-Stock Corporation “Vympel”, Moscow,

Further development of modeling of spatial distribution of energetic electron fluxes near Europa M. V. Podzolko 1, I. V. Getselev 1, Yu. I. Gubar 1, I.

Babakin Space Center, Space Research Insitute, Makeev Rocket Design Bureau COSMOS ONE: THE FIRST SOLAR SAIL a project of The Planetary Society with Cosmos.

1 Winter Launch Block Modeling and Results MMS Flight Dynamics Team MIWG 8 Feb. 20, 2014.

Ballistics and navigation support for the Venera-D mission V. A. Shishov 1, V. A. Stepaniants 1, A. G. Tuchin 1, S. M. Lavrenov 2 (1)Keldysh Institute.

MSU Space Project «Lomonosov». MSU Space Project «Lomonosov» Participants of the experiment (preliminary list): M.V. Lomonosov Moscow State University.

16 years of LAGEOS-2 Spin Data from launch to present Daniel Kucharski, Georg Kirchner, Franz Koidl Space Research Institute Austrian Academy of Sciences.

Remote Sensing of the Ocean and Atmosphere: John Wilkin Orbits and Measurement Geometry IMCS Building Room 214C ext 251.

Chpt. 5: Describing Orbits By: Antonio Batiste. If you’re flying an airplane and the ground controllers call you on the radio to ask where you are and.

Liulin-F charged particle telescope for radiation environment investigation aboard Phobos-Grunt interplanetary spacecraft SES 2010, Sofia, 2-4 November,

AT737 Satellite Orbits and Navigation 1. AT737 Satellite Orbits and Navigation2 Newton’s Laws 1.Every body will continue in its state of rest or of uniform.

Method of Virtual Trajectories for the Preliminary Design of Multiple Gravity-Assist Interplanetary Trajectories Sergey Trofimov Keldysh Institute of Applied.

Samara State Aerospace University (SSAU) Samara 2015 SELECTION OF DESIGN PARAMETERS AND OPTIMIZATION TRAJECTORY OF MOTION OF ELECTRIC PROPULSION SPACECRAFT.

1 Samara State Aerospace University (SSAU) Modern methods of analysis of the dynamics and motion control of space tether systems Practical lessons Yuryi.

Optimal Low-Thrust Deorbiting of Passively Stabilized LEO Satellites Sergey Trofimov Keldysh Institute of Applied Mathematics, RAS Moscow Institute of.

© Lavochkin Association, 2013 Ganymede Lander mission overview.

What can you tell me about gravity?. Gravity is usually assumed to be a uniform vertical downward force......it is actually radial.

факс: +7 (846)

University of Colorado Boulder ASEN 5070: Statistical Orbit Determination I Fall 2014 Professor Brandon A. Jones Lecture 3: Basics of Orbit Propagation.

“Good Practices” for long term orbit propagation and associated criteria verification in the frame of the French Space Act Presentation.

A Brief Introduction to Astrodynamics

Chapter 5 Circular Motion; Gravitation. 1. Use Newton's second law of motion, the universal law of gravitation, and the concept of centripetal acceleration.

Team 5 Moscow State University Department of Mechanics and Mathematics I.S. Grigoriev, M.P. Zapletin 3rd Global.

V.V.Sidorenko (Keldysh Institute of Applied Mathematics, Moscow, RUSSIA) A.V.Artemyev, A.I.Neishtadt, L.M.Zelenyi (Space Research Institute, Moscow, RUSSIA)

Chapter 10 Forces Objects will not begin to move or change motion until an unbalanced force acts on it. Newton’s 1st Law of Motion Inertia All mass resists.

Gravitational Field Historical facts Geocentric Theory Heliocentric Theory – Nicholas Copernicus (1473 – 1543) Nicholas Copernicus – All planets, including.

7-6 Solving Natural Log Equations

Low Thrust Transfer to Sun-Earth L 1 and L 2 Points with a Constraint on the Thrust Direction LIBRATION POINT ORBITS AND APPLICATIONS Parador d'Aiguablava,

The Third Moscow International Solar System Symposium. Moscow, 8-12 October MS 3 -MN-11 LANDING DYNAMICS ON THE «LUNA-GLOB» PROJECT Sikharulidze.

Space : missions and telescopes. Space missions PASTMERCURY GEMINI APOLLO SPACE SHUTTLE World War 2 A2 1 st soviet in orbit.

MAE 4262: ROCKETS AND MISSION ANALYSIS

What Makes Up the Space Shuttle? The space shuttle is the most complex machine ever created by human beings. The first shuttle was launched on April 12,

Sea Launch/Zenit Thrust: 8,180,000 N Fueled Weight: 450,000 kg Payload to LEO: 13,740 kg Cost per launch: $100,000,000 Cost per kg: $7,300 Launches: 31/28.

© ИАЦ КВНО ЦНИИмаш Собственность ИАЦ. All rights reserved GLONASS Status and Progress Sergey Revnivykh CGSIC Meeting , Savannah, GA, US.

Van Allen Extended Mission Orbit Analysis 9/2014 SWG T. Sotirelis, F. Siddique JHU/APL.

Results of GEO and HEO monitoring by ISON network in th session of STSC COPUOS Vienna Feb 2013 Russian Academy of Sciences Keldysh Institute.

XUV monochromatic imaging spectroscopy in the SPIRIT experiment on the CORONAS-F mission I. Diagnostics of solar corona plasma by means of EUV Spectroheliograph.

THEMIS MIWG #3Probe Separation Analysis - Page 1June 15 & Probe Separation Analysis Daniel Rummel UCB.

PHYSICS 1010 Spring James Stucki Randall Forbush James Roundy Daniel Renzo

INFORMATION SUPPORT SYSTEM OF THE SOLAR SAIL MISSION: PRACTICAL ASPECTS. Nazarov, V. 1 ; Gotlib V. 1 ; Lipatov A. 1 ; Bashe, I. 2 ; Korotkov, F. 1 ; Markov,

ABOVE THE ATMOSPHERE AND UNDER CONTROL Topic 6. Rockets – Getting Up There The science of rocketry relies on a basic physics principle that you learned.

Different scenarios of the “Venera-D” mission KIAM Ballistic Center Team (Keldysh Institute Of Applied Mathematics RAS)

Astronomical Institute University of Bern 1 Astronomical Institute, University of Bern, Switzerland * now at PosiTim, Germany 5th International GOCE User.

Igor Molotov Keldysh Institute of Applied Mathematics RAS,

Environment Simulator

Deployment Optimization for Various Gravitational Wave Missions

Lunar Trajectories.

Kinematics 1D Motion Problem Set.

Technical Resource Allocations

Mikhail Koptev Yaroslav Mashtakov Mikhail Ovchinnikov Sergey Shestakov

Current status of the ISON optical network

Vladimir Agapov, Igor Molotov, Victor Stepanyants

Theory of Quasi-Electrostatic Waves in a Magnetoplasma Applied to Antenna Measurements on Board Rockets and Satellites Evgenii A. Shirokov Institute of.

LAUNCH OF GEO STATIONARY SATELLITES

T. Schildknecht, A. Vananti, A. Hinze

Universal Gravitation

ISRS2007, Lamada Plaza Hotel, Jeju, Korea, 31 October - 2 November 2007 Radargrammetry of High-Resolution Synthetic Aperture Radar A Theoretical Study.

Solving Quadratic equations by graphing.

Apollo and Beyond.

PROBA 2 orbits and conditions of EUV observations V. Slemzin P. N

7-th European Space Debris Conference 2017

The role of seismic tomography for the Earthquake Early Warning system

“The First year of HEND operations on the NASA Odyssey Mars Orbiter”

Presentation transcript:

TRACKING OF PHOBOS-GRUNT MISSION IN LOW EARTH ORBIT Alexander S. Samotokhin, Andrey G. Tuchin M.V. Keldysh Institute of Applied Mathematics of Russian Academy of Sciences, Moscow, Russia Sergey A. Sukhanov, Zakhary N. Khutorovsky, Andrey V. Rykin Interstate Joint-Stock Corporation “Vympel”, Moscow, Russia

2 On-Earth control structure of Phobos-Grunt mission

3 The schedule of LEO operations OperationTime, MskNote Launch to base orbit00:16: :18:28.7Separation of spacecraft from 2nd stage of the rocket Base orbit00:18: :55:47.9Hp=207 km Ha=347 km 1st maneuver02:55: :05:18.2  V=815.7 m/s Separation of external tank Intermediate orbit03:05: :02:48.8Hp=244 km Ha=4162 km 2nd maneuver05:02: :20:09.9  V= m/s

4 The trace of Phobos-Grunt in low Earth orbits

5 Relative movement of PG and (SGP4 model)

6 Relative movement of PG and (SGP4 model, compensation of time error is applied)

7 The evolution of A/m ratio (Nov 9 – Dec 10)

8 Analyzed orbital parameters The draconic period (the time that elapses between two passages of the object through its ascending node) The height of perigee The latitude of under-satellite point in perigee Considered parameters are not osculated elements. These parameters were calculated during one revolution with use of the corresponding propagator. The designations used in subsequent figures The propagated evolution Actual Russian SSS data Actual American SSS public data (TLE)

9 Evolution of the orbit parameters Nov 9-22 passive movement, A/m= m 2 /kg (nominal)

10 Evolution of the orbit parameters Nov 9-Dec 6 passive movement, A/m= m 2 /kg (nominal)

11 Evolution of the orbit parameters Nov 9-22 passive movement, A/m= m 2 /kg (58% nominal)

12 Evolution of the orbit parameters Nov 9-22 nominal A/m, acceleration along velocity: 2.83∙10 -6 m/sec 2

13 Evolution of the orbit parameters Nov 9-22 accelerations: along velocity: 2.49∙10 -6 m/sec 2, s/c-Sun direction 1.16∙10 -5 m/sec 2

14 Conclusions 1.Really space surveillance systems were the only source of information about behavior of Phobos-Grunt onboard systems in low Earth orbit. It is a very unusual situation. 2.The data both Russian and American SSS proves that the movement of Phobos-Grunt were not passive during the first days after the launch. These data allowed to obtain a estimation of actual perturbations. 3.The interaction between on-Earth control structure of the mission and Space surveillance system was unsatisfactory. It is necessary to provide real time data exchange between these systems in the future.