A new approach to air traffic controller workload measurement and modelling
Obstacle avoidance for small UAVs using monocular vision
A TMO-based flight program of an unmanned helicopter
Vibrational genetic algorithm enhanced with neural networks in RCS problems
A feature-assisted matching algorithm for lunar rover
Fuel system design of the smart UAV considering operational reliability
Free vibration analysis of a rotating Timoshenko beam by differential transform method
Iterative solution to differential geometric guidance problem
The operational efficiency of passenger aircraft
A simulation environment for design and testing of aircraft adaptive fault-tolerant control systems
A new method for design cycle period management in aircraft design process
Direct adaptive fuzzy control for a nonlinear helicopter system
Control system design of multivariable non-linear space robots
The robust adaptive attitude control of a certain satellite
An almost disturbance decoupling solution of the attitude control problem
Relative dynamics and initialization condition of spacecraft formations in eccentric orbits
Re-aligning of further and higher education with the aircraft engineering sector
Investigation of process parameters in superplastic free bulge forming
RHC-based attitude control of spacecraft under geometric constraints
Estimation method combining aircraft kinematics, GPS, and low-quality rate gyros
Validation of comprehensive dynamics analysis predictions for a rotor in descending flight
Optimization of geometric parameters of latticed structures using genetic algorithm
Enhanced method for single-antenna GPS-based attitude determination
A study of solar-powered, high-altitude unmanned aerial vehicles
Simple autopilot design procedure based on a factorization approach
Analysis and optimisation of a MALE UAV loaded structure
Simple virtual attitude sensors for general aviation aircraft
Structural design and test capability of an integrated stiffened CFRP panel
Improving future air traffic punctuality: "pinch-and-pull" target windows
Boundary layer effects on a wing in ground-effect
The flying laboratory for aeronautics students' education
Configurations analysis for high-altitude/long-endurance airships
Design and analysis for an innovative scheme of SINS/GPS ultra-tight integration
Fast trajectory planning based on in-flight waypoints for unmanned aerial vehicles
Rotorcraft research in India: recent developments
Energy and emission assessments of continuous descent approach
Design and reliability prediction of a distributed landing gear control system
The cheap air data computer for aviation applications
Dynamic loading systems for ground testing of high speed aerospace actuators
MALE UAV design of an increased reliability level
Spacecraft vibration reduction using pulse modulated command input and smart materials
Development of methods identifying parameters in reaction wheel assembly disturbance model
Flight control system design for a micro aerial vehicle
Configurations analysis for high-altitude/long-endurance airships
Induced rolling moment for NACA4412 plain and flapped wing
Design and reliability prediction of a distributed landing gear control system