Transactions of Nanjing University of Aeronautics and Astronautics
- Flight Control System of Unmanned Aerial Vehicle
- UAV Velocity Measurement for Ground Moving Target
- Gyroscope Fault Diagnosis Using Fuzzy SVM to Unbalanced Samples
- Recent Progress in Heavy Fuel Aviation Piston Engine
- Nonlinear Intelligent Flight Control for Quadrotor Unmanned Helicopter
- Guidance and Control for UAV Aerial Refueling Docking Based on Dynamic Inversion with L1Adaptive Augmentation
- Wind Estimation for UAV Based on Multi-sensor Information Fusion
- Adaptive Human Tracking Across Non-overlapping Cameras in Depression Angles
- Transonic Rudder Buzz on Tailless Flying Wing UAV
- Control-Oriented Modeling and Simulation on Rigid-Aeroelasticity Coupling for Hypersonic Vehicle
- Flight Dynamic Analysis of Hypersonic Vehicle Considering Liquid-Solid Coupling
- Tradeoff Analysis of Factors Affecting Longitudinal Carrier Landing Performance for Small UAV Based on Backstepping Controller
- Improved Shuffled Frog Leaping Algorithm Optimizing Integral Separated PID Control for Unmanned Hypersonic Vehicle
- CRB for 2-D DOA Estimation in MIMO Radar with UCA
- High Velocity Impact Experiment on Ti/CFRP/Ti Sandwich Structure
- Beamforming of Whole Airspace Phased Array TT&C System Based on Linear Subarrays
- Trim Drag Prediction for Blended-Wing-Body UAV Configuration