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Flight Dynamics
1002-0853
2014 Issue 4
Influence of ground effect on aircraft dynamic characteristics during ultra-low altitude airdrop
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page:289-293
Application and research of the pilot optimal control model
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page:294-297,302
Analysis of unloading characteristics of the canard rotary wing airplane blade in transitional process
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page:298-302
Construction-method of irregular microburst with turbulence effect
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page:303-307
Analysis for drag characteristic of variable swept wing-body
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page:308-311
Study on UAV's trimming strategy for single aileron jammed at a large angle
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page:312-314
Beyond visual range air combat simulation of UAV based on improved two-step adjudication method
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page:315-319,324
Investigations of impact on drag coefficient of drogue canopy caused by the number of drogue strut in aerial refueling system
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page:320-324
Sliding mode variable structure control law design for hypersonic vehicle
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page:325-328
Method for soft switching of re-entry vehicle's robust controllers
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page:329-333
Analyze and simulation on the characteristics of spacecraft resonance orbit
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page:334-337
Autonomous orbit maintenance strategy for relative phase of MEO satellite
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page:338-341,346
Optimization technique of frequency domain response identification
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page:342-346
Study on the large size high altitude propeller aerodynamic performance test method
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page:347-350,355
Probe into landing configuration "peck" and automatic dive
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page:351-355
Analysis of coaxial helicopter vortex ring characteristics
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page:356-359
Trimming for aircraft's glide based on an improved artificial fish-school algorithm
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page:360-363,367
Application of genetic algorithm based control allocation in airship
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page:364-367
Particle swarm optimization for dynamic resource allocation in UAV cooperative attack
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page:368-371,375
Simulation of pursuit-evasion resistance based on differential game
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page:372-375
Risk probability assessment for hose-paradrogue of the aerial refueling by extreme value theory
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page:376-379,384
Study on method of risk probability index determination in aircraft system safety analysis
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page:380-384