Folding Large Orbital Complexes Radio Antennas Kosmosurisistemebis

By Tserodze, Shota

Book Id: WPLBN0003841617
Format Type: PDF eBook:
File Size: 0.1 MB
Reproduction Date: 2015

Title:	Folding Large Orbital Complexes Radio Antennas Kosmosurisistemebis
Author:	Tserodze, Shota
Volume:
Language:	Georgian
Subject:	Georgian, Antennas and Microwave Frequency, Engineering & Allied Operations
Collections:	European Libraries Collection, National Library of Georgia Collection
Historic Publication Date:	2006
Publisher:	Library of Georgia


Citation APA MLA Chicago Tserodze, B. S. (2006). Folding Large Orbital Complexes Radio Antennas Kosmosurisistemebis. Retrieved from http://gutenberg.cc/

Table of Contents
TOC: Chapter 1. Using Large Deployable Antennas and Satellite Systems; 1.1. Satellite Communications; 1.2. Radio; 1.3. Remote Sensing; 1.4. Emergency Communications; 1.5. Earth Observation; 1.6. Energy Production and Transmission; 1.7. Large Items Reflectors Radio Complexes and their Use of Space Technology For Military Engineering; 1.8. Tsibovan-Kolgisebri Constructive Analysis and Circular Reflectors; Chapter 2. Getting the New Solutions and their Constructive Analysis Paraboloiduri Shape. 2.1. Adoption of Thin-Walled Hollow Structures Pormattsarmomkmneli Light Kolguri Type of Concentric Tubes Drekadplastiuri Properties Using 2.1.1. Gaghunulgheroebiani Adjustable Light Membrane Structure Pormattsarmomkmneli Structure: 2.1.2. Construction of the Local Light Gaghunulgheroebiani Membrane Stretching the Point: 2.1.3. Construction Iribana Mchimebit Light Gaghunulgherovani Prospects: 2.2. Construction of the Power Pantograpit Paralelurtsiboebiani Arakontsentruli Arc: 2.3. Ring Systematic Mechanical Structures; 2.3.1. Single-Layer Pantograpuli Basic Constructs and Chasaketsi Levers; 2.3.2. Single-Layer Pantograpuli Constructs Chasaketsi Levers; 2.4. Orbital Station Mir the Experiment Reflector; Chapter 3. European Large Deployable Reple- Ktorebis (Ldr) and Construction of the Logic of the Program; 3.1. Structural Analysis of the Charts and A Brief Description; 3.1.1. Abbreviations, Flow Diagrams and Basic Requirements; 3.1.2. Power Link (Ria); 3.1.3. Power Levers (Ptl); 3.1.4. Pantograpis Scaffoldings (Pts, Pns); 3.1.5. Locking Mechanism (Rls); 3.1.6. Suspension Rdm; 3.1.7. Bagiruli System (Tds); 3.1.8. Torque (Fs) and Geometry (Gs) Sensors; 3.1.9. Potentiometric Sensors (Ds); 3.1.10 Society. Console System (Ces); 3.1.11. Radial Sheets (Rar); 3.1.12. the Central Node (Cei); 3.1.13 Society. Reflective Surface (Rsm); 3.1.14. Removal of the Containment System (Rhs); 3.1.15. Cash Flow From the Containment Ring Or Laid Stabilizing System (Rhr); 3.1.16. the Rigidity of the System (Sts); 3.2. Ldr-1- and Evm-2-'S Geometric, inertial Mass and Characteristics; 3.3. Ldr-1 and Evm-2 Plate Constructions (Ura) Description; 3.3.1. the Central Node (Cei); 3.3.2 System Radial Sheets (Rar); 3.3.3 Additional Sheets System (Srs) (only For Evm-2-); 3.3.4. Power Link; 3.3.5. Element Console System (Ces); 3.3.6. the Spreading of the Power System Components; 3.3.7. Electromechanical Power Drive Unit (Rdm) Ldr-1 and Evm-2 Options; 3.3.8. Reflective Surface (Rsm); 3.3.8.1. Reflective Surface (Rsm) Design and Technical Characteristics; 3.3.8.2. Reflective Surface Fastening Elements; 3.3.9. Cash Flow From the Power Unit of the Containment System (Rhr) (only Ldr 2-A); 3.3.10. the Rigidity of the System (Sts); 3.3.11. Ura-'S System of Checks and Commissioning Stage of Withdrawal (Rhs); 3.4. Ldr-1 and «Evm» -2 Construction of A Comparative Analysis of the Basic Parameters; 3.4.1. Step By Step Description of the Operation of Radio Systems; 3.4.2. Ldr-1 and Evm-2 Variants of the Basic Parameters of the Comparison; 3.4.2.1. Construction of the Possible Impact on the Grid Stretching Forces; 3.4.2.2. Kinematic Features of the Scheme; 3.4.2..3. Escalation of the Number of Actuators Required For Active; 3.4.2.4. Operation of the Tension Elements; 3.4.2.5. Geometry Control Than Usual; 3.4.2.6. Relative Movement Between the Elements of the Possible Risks Refleqtoris Fashion; 3.4.2.7 the Duration of the Deployment Process; 3.4.2.8. Reflective Surface Shape Accuracy; 3.4.2.9. Ura-'S Hardness (their Frequency Values); 3.4.2.10. Dimensions of Transport Packages; 3.4.2.11. Weights-inertial Characteristics; 3.4.2.12 Manufacturing Processes and Assumptions Krizisuloba; 3.4.2.13. Procedures and Assumptions Krizisuloba Plate Assembled; 3.5. the Spreading of the Kinematic Analysis of the Factors Impeding the Ldr-1 and Evm-2 Options; 3.5.1. Ldr-1 Option; 3.5.2. Evm -2 Option; 3.6. Large Deployable Reflector Surface Ldr- Real Geometric Rate; 3.6.1. Test Strategy and Technical Requirements; 3.6.2. Fixing Antigravitatsiul Reflector System and Its Open-Folding of Multiple Test; 3.6.3. Real Geometric Shape Rate; 3.6.3.1. Photogrammetry Methods; 3.6.3.2. Scanning Systems; 3.6.3.3. Multiteodolitis Technology; 3.6.3.4. Surface Adjustment; 3.6.4. Passive intermodulatsiis (Pim) inspection Measures; Chapter 4. the Final Design of Large Space Reflector Logic and theoretical Analysis; 4.1. Ring and the Synthesis of Large Aerospace Systems Tsibovan-Umbrella Reflector Structure; 4.1.1. Evm -2-'S Gradual Improvement and Construction of Logic; 4.1.2. Generalized Description of the Possible Variants of Construction; 4.1.3. Evm -2- Advantages in Ensuring the Accuracy of the Reflectors; 4.1.4. offset Reflectors With A Satellite Connection and Orientation Schemes; 4.2. Evm -2- theoretical Analysis; 4.2.1. the Spreading Process Analysis; 4.2.1.1. A Mathematical Model of the Process of Setting Up A Reflector; 4.2.1.2. the Spreading of the Results of the Analysis; 4.2.2. Analysis of Stress-Strained State; 4.2.2.1. A Mathematical Model of Large Deployable Reflector; 4.2.2.2. Reflector Stress-Strained State of the Analysis Results; 4.2.2.3. Conclusions Dynamic Parameters of the Reflector; 4.2.2.4. the Results of Stress-Strained State of Impacts of Temperature Loads; 4.3. offset Reflector Reflective Surface Electromagnetic Waves Delivery Parameters For Accuracy; 4.3.1. in theory, A Mathematical Analysis of the offset Surfaces; 4.3.2. Least Squares Method Tsarmosakhuiti Maproksimirebeli Function Parameters: 4.3.3. offset Antenna Grid Surface Imaginary and theoretical Calculation of the Mean Square Deviation Paraboloidebis Mimaprt: 4.3.4. offset Reflector Grid Reflective theoretical Upper Limit of the Average Square Deviation Rate and Natenis Surface Dots of Different Size Ujredebiani Bijebisa Accuracy Appointment For Further Evaluation: 4.4. Space-Based Systems For Transforming Spatial Geometry, Structural and Kinematic Analysis; 4.4.1. Hyperbolic Surface Structure and Kinematic Analysis of Transforming the System; 4.4.1.1. Stem Structure of the System; 4.4.1.2. Transforming the System of Setting the Geometric Characteristics; 4.4.1.3. Kinematic Analyzes of the Ring Element. 4.4.1.4. Rational Basic Kinematic Chain Transforming Systems; 4.4.1.5. Basic Kinematic Chain of the Main Geometric Parameters. Funds Reporting Model; 4.4.1.6. Ring System Reporting Model; 4.4.2. Elliptic Cone and Transforming the Structure and Kinematic Analysis Systems; 4.4.2.1. Cone Ring Mechanism Basic Geometric Parameters; 4.4.2.2. Facility-Level Structure; 4.4.2.3. Two Conical Structure and Kinematic Analysis Rgoliani Transforming System; 4.4.2.4. Elliptic Rgoliani Transforming Geometric Analysis System; Chapter 5. Experimental Studies; 5.1. Evm-2 Power Ring and the Diametrically Disposed Radial Reflector Manufacturing and Testing of Experimental Models of the Fragment; 5.1.1. Evm-2 Power Ring Reflector Manufacturing and Testing of An Experimental Model of Transformation; 5.1.2. Evm-2 Diametrically Disposed Radial Reflector Fragments in Manufacturing and Testing of Model Experiments Passion; 5.2. Makhvilmimartuli Space Basing of Large Antennas For Earth Remote Zone of the Test Method For Radio Communication; Conclusions; Literature; Annexes.