9.1.3 Technical Characteristics of Electric-Hydraulic
Servo System for Aircraft . . . . . . . . . . . . . . . . . . . . . . 65
9.1.4 Design Method of Air Defense Missile Control
Execution System . . . . . . . . . . . . . . . . . . . . . . . . . . . . 76
9.1.5 Auxiliary Energy for Air Defense Missiles . . . . . . . . . . 95
9.1.6 Hydraulic Energy Application Technology
of Gas Turbine Pump for Aircraft . . . . . . . . . . . . . . . . 110
9.2 Power Matching Design of Steering System . . . . . . . . . . . . . . . 115
9.2.1 Load Model of Steering System . . . . . . . . . . . . . . . . . 115
9.2.2 Optimal Matching of Output Characteristics
and Load Trajectories of Servo Mechanism . . . . . . . . . 119
9.2.3 Energy Demand of Actual Steering System . . . . . . . . . 121
9.2.4 Variation Factors of Working Pressure
and Frequency Characteristics of System . . . . . . . . . . . 122
9.3 Design Principle of Gas Generator . . . . . . . . . . . . . . . . . . . . . . 123
9.3.1 Theoretic Derivation . . . . . . . . . . . . . . . . . . . . . . . . . . 124
9.3.2 Application Discussion . . . . . . . . . . . . . . . . . . . . . . . . 129
9.4 Design Principle of Small Gas Turbine for Missile . . . . . . . . . . 135
9.4.1 Thermodynamic Process in Small Gas Turbine
Nozzle for Missile . . . . . . . . . . . . . . . . . . . . . . . . . . . 135
9.4.2 Efficiency of Small Gas Turbine in Missile
Hydraulic System . . . . . . . . . . . . . . . . . . . . . . . . . . . . 140
9.4.3 Graphical Analysis Method for Stress of Small
Gas Turbine Disk for Missile . . . . . . . . . . . . . . . . . . . 144
9.5 Starting Characteristics of Electronic and Hydraulic
Power Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 151
9.5.1 Description of EHPU Starting Characteristic . . . . . . . . 151
9.5.2 EHPU Theoretical Modeling . . . . . . . . . . . . . . . . . . . . 152
9.5.3 Starting Characteristics of Hydraulic System . . . . . . . . 154
9.5.4 Starting Characteristics of Power Supply System . . . . . 156
Bibliography . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 159
10 Application of Aerodynamic Technology in Attitude Control
of Aerocraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 163
10.1 Aerodynamic Attitude Control Principle and Attitude
Control Method of Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . 164
10.1.1 New Method and Principle of Attitude Control
of Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 164
10.1.2 Lateral Force Analysis of Attitude Control . . . . . . . . . . 166
10.1.3 Experiments and Analysis . . . . . . . . . . . . . . . . . . . . . . 169
10.1.4 Conclusions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 175
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