Abstract |
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xiii | |
Preface |
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xv | |
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1 Computer Simulation in Aircraft |
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1 | (22) |
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1.1 Simulation of Aircraft |
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1 | (2) |
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3 | (2) |
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1.3 Modeling of Streamlined Surfaces |
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5 | (1) |
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1.4 Simulation of the Be-200 Amphibious Aircraft |
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6 | (3) |
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1.5 Conceptual Model of Aircraft "Chiroptera" |
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9 | (5) |
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1.6 Conceptual Design of "Lotos" Motorcar |
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14 | (5) |
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19 | (4) |
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2 Conceptual Modeling of Amphibian Aircrafts |
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23 | (114) |
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2.1 From the History of World Civil Aviation |
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24 | (6) |
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24 | (1) |
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2.1.2 Historical Stages of Hydroaviation Development by the Beriev Aircraft Company |
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25 | (5) |
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2.2 Computational Modeling of Multipurpose Amphibious Aircraft Be-200 |
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30 | (8) |
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30 | (1) |
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2.2.2 Modeling Methods and Stages |
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31 | (4) |
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2.2.3 Shading of 3D Model |
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35 | (1) |
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2.2.4 Rendering of 3D Model |
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36 | (2) |
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38 | (1) |
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2.3 Computational Modeling of Passenger Amphibian Aircraft Be-200 Cabin Interior |
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38 | (12) |
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38 | (2) |
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2.3.2 Variants of Cabin Layout |
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40 | (3) |
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2.3.3 Aircraft Cabin Modeling |
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43 | (2) |
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2.3.4 Shading of Aircraft Cabin Objects |
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45 | (2) |
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2.3.5 Rendering of Aircraft Cabin |
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47 | (1) |
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48 | (2) |
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2.4 Computational Modeling of Amphibious Aircraft Be-103 |
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50 | (10) |
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50 | (1) |
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2.4.2 Modeling Methods and Stages |
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51 | (5) |
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2.4.3 Shading of 3D-Model |
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56 | (2) |
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2.4.4 Rendering of 3D-Model |
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58 | (2) |
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60 | (1) |
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2.5 Conceptual Model of "Lapwing" Amphibious Aircraft |
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60 | (14) |
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60 | (1) |
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2.5.2 Concept Development |
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61 | (7) |
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2.5.3 3D Modeling of Amphibious Aircraft "Lapwing" |
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68 | (3) |
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2.5.4 Shading and Rendering of 3D Model of "Lapwing" Amphibious Aircraft |
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71 | (3) |
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2.6 Computational Modeling of the Cabin Interior of the Conceptual Model of Amphibian Aircraft "Lapwing" |
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74 | (11) |
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74 | (1) |
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2.6.2 The Concept of the Amphibian Aircraft "Lapwing" |
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75 | (2) |
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77 | (1) |
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2.6.4 Development of a Passenger Seat |
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78 | (3) |
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2.6.5 Modeling of the Cabin Interior |
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81 | (1) |
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2.6.6 Assignment of Materials and Rendering of the Scene |
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81 | (2) |
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2.6.7 Usability and Comfort Cabin Interior |
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83 | (2) |
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85 | (1) |
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2.7 Conceptual Model and Interior Design "Water Strider" Ekranoplan |
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85 | (23) |
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85 | (1) |
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2.7.2 Review of Ekranoplans |
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86 | (6) |
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2.7.3 Review of Publications |
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92 | (1) |
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2.7.4 Concept of an Ekranoplan of "Water Strider" |
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93 | (3) |
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2.7.5 Configuration of the Concept of an Ekranoplan |
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96 | (1) |
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96 | (4) |
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2.7.7 Shading and Rendering of Model |
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100 | (1) |
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2.7.8 Development of an Interior and Passenger Chair |
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101 | (3) |
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2.7.9 Creation of Materials and Rendering of an Interior |
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104 | (3) |
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107 | (1) |
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2.8 Design of Multifunctional Hydrofoil "Afalina" |
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108 | (11) |
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108 | (1) |
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109 | (3) |
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2.8.3 Development of the Concept |
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112 | (2) |
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114 | (1) |
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2.8.5 Shading and Rendering of the Model |
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115 | (4) |
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119 | (1) |
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2.9 Autonomous Mobile Robotic System "Sesarma" |
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119 | (10) |
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119 | (1) |
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2.9.2 Review of Publications |
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119 | (1) |
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2.9.3 Review of the Analogues |
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120 | (1) |
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121 | (2) |
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123 | (1) |
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123 | (3) |
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2.9.7 Creation and Assignment of Materials |
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126 | (2) |
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2.9.8 Lighting Installation and Rendering |
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128 | (1) |
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129 | (1) |
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129 | (8) |
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3 Development of Schemes of Multirotor Convertiplanes with Cryogenic and Hybrid Powerplants |
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137 | (24) |
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137 | (1) |
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3.2 Hydro Convertiplane is the New Opportunity for Modern Aviation |
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138 | (5) |
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3.3 Peculiarities of Control of the Vertical Takeoff and Landing Aircraft in the Transitional and Hovering Mode |
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143 | (5) |
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3.4 Problems of Stability and Controllability of Hydro Convertiplane with Tandem-Mounted Rotors in Rotary Annular Channels |
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148 | (2) |
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3.5 Cryogenic Turboelectric Aircrafts are a Good Solution for Short-Range and Takeoff Hybrid Airline Complexes |
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150 | (4) |
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154 | (4) |
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158 | (3) |
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4 Conceptual Design of A Multifunctional Amphibious Plane |
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161 | (18) |
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4.1 Introduction, Historical Stages |
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161 | (6) |
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167 | (3) |
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170 | (1) |
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4.4 Application of Materials, Rendering |
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171 | (5) |
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176 | (1) |
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176 | (3) |
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5 Mathematical Model of Unmanned Aircraft with Elliptical Wing |
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179 | (32) |
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180 | (1) |
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180 | (1) |
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181 | (1) |
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5.4 Hardware Implementation |
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181 | (2) |
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5.5 The Program Research Part |
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183 | (1) |
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5.6 Studies of the Behavior of an Unmanned Aircraft with an Elliptical Wing |
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184 | (3) |
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5.7 Experimental Studies of the UA Behavior |
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187 | (2) |
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5.8 Processing and Analysis of Data Obtained during Flight Tests |
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189 | (4) |
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5.9 Formation of a Mathematical Model of UA with Elliptical Wing |
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193 | (1) |
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5.10 Mathematical Model of UA in Analytical Form |
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193 | (2) |
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5.11 Obtaining a Mathematical Model using the "Black Box" Method |
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195 | (2) |
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5.12 Mathematical Model Based on Linear Regression |
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197 | (3) |
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5.13 Mathematical Model Based on Multilayer Perceptron |
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200 | (1) |
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5.14 PID Controller Setup |
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201 | (2) |
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5.15 Flight Emulation for Primary Quality Control of the Regulator |
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203 | (2) |
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205 | (3) |
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208 | (3) |
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6 Technology of Geometric Modeling of Dynamic Objects and Processes of Virtual Environment for Aviation-Space Simulators Construction |
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211 | (50) |
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211 | (5) |
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6.2 Methods of Applied Geometry in Solving Problems of Simulation Modeling in SVR |
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216 | (13) |
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6.2.1 Optimum Discretization of Curved Lines |
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217 | (4) |
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6.2.2 Curve Integral Model |
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221 | (1) |
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6.2.3 Methods for Assessing the Information Capacity of Discrete Curve Frames |
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222 | (2) |
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6.2.4 Optimal Discretization Based on Integral Curve Model |
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224 | (5) |
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6.3 Purposes and Objectives of the Extravehicular Activity of the RTS Cosmonaut Operator on the ISS in Open Space, Technology of Computer Simulation in the Virtual Reality Environment |
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229 | (12) |
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6.3.1 Extravehicular Activity of the RTS Cosmonaut Operator |
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229 | (3) |
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6.3.2 Technologies of Methodical and Hardware-Software Implementation of a Cosmonaut-Operator's Simulator |
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232 | (3) |
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6.3.3 Dynamic Virtual Model of the Manipulator |
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235 | (4) |
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6.3.4 Software Technologies for the Formation of Dynamic Models of the Editor-Modeler |
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239 | (2) |
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6.4 Experimental Studies of the Functional Completeness of TMS Graphics and Software |
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241 | (14) |
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6.4.1 Information and Functional Power of the TMS Visualizer |
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241 | (3) |
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6.4.2 An Example of a Simulator of a Typical Flight Mission at Solar Battery Installation |
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244 | (4) |
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6.4.3 The Technology of Testing Emergency Situations |
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248 | (6) |
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6.4.4 Experimental Search for a Safe Trajectory of ERA Movement |
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254 | (1) |
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255 | (3) |
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258 | (3) |
Index |
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261 | |