Flight Dynamics 2014 Issue 5 Variable stability control and variable capability evaluation of a helicopter

Home | Survey | Payment| Talks & Presentations | Job Opportunities

Journals A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Flight Dynamics
1002-0853
2014 Issue 5

Variable stability control and variable capability evaluation of a helicopter

..............page:385-388,402

Research on aerodynamic effect modelling of receiver based on numerical simulation of wake vortex

..............page:389-393

Elastic model for high aspect ratio airplane landing impact analysis

..............page:394-397,402

Dynamics modeling and simulation of heavy-equipment airdrop multi-body system

..............page:398-402

Modeling and simulation of air-breathing hypersonic vehicles separation dynamics

..............page:403-407

Nonlinear dynamics analysis of the hypersonic vehicle

..............page:408-412

Flight dynamics modeling and analysis of hypersonic flight vehicle in gust wind

..............page:413-417

Self-repairing control law design of aircraft longitudinal maneuver

..............page:418-422

Design of RHO controller for morphing aircraft based on command filter

..............page:423-426,431

Design and simulation of fuzzy sliding mode controller of quadrotor aircraft

..............page:427-431

Design of optimal pursuit and evasion guidance law for active protection

..............page:432-436

Reconfigurable control of reusable launch vehicles

..............page:437-440,454

Analytical solution of the relative motion and optimal control for the approach phase of spacecraft docking

..............page:441-445,454

Failure simulation of actuator for suborbital reusable launch vehicle return course

..............page:446-449

Impulsive optimization control based orbital transfer correction

..............page:450-454

Closed-loop inverse kinematic control schemes for free-floating space robot

..............page:455-459

ARJ21-700 aircraft WAI natural icing flight test approach

..............page:460-463

A lateral state-space model based on the idea of splitting the aircraft into several lifting surfaces or panels

..............page:464-467,476

Research of slipstream effect on fuselage upside installed single-propeller-driven aircraft

..............page:468-471

Integrated index model for cooperative air combat effectiveness assessment of manned/unmanned vehicles

..............page:472-476

Research on methods of air combat threat evaluation under inaccurate information

..............page:477-480