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1. Manikin study showed that neonates are exposed to high sound and vibration levels during helicopter incubator transports.

2. Construction of Power Line Inspection System Using a Quadrotor Helicopter.

3. Optimal Transition of Coaxial Compound Helicopter after Total Propeller Failure.

4. Development aspects of cable cutter cartridge for helicopter application.

5. Radar detectability of light aircraft micro‐Doppler modulation.

6. An Improved Iterated Greedy Algorithm for Solving Collaborative Helicopter Rescue Routing Problem with Time Window and Limited Survival Time.

7. Adaptive fault‐tolerant control of a nonlinear 2‐DOF helicopter system with prescribed performance.

9. Numerical simulation of ice accretion on helicopter rotor blades with trailing edge flap.

10. Dynamic Stall Alleviation of a Helicopter Blade Section in Forward Flight Condition Using an Optimized Combination of Active Nose Droop and Active Gurney Flap.

11. Development of a Mathematical Model of a Coaxial Compound Helicopter for Trimming and Stability Analysis.

12. Incremental Sliding Mode Control for Predefined-Time Stability of a Fixed-Wing Electric Vertical Takeoff and Landing Vehicle Attitude Control System.

13. HeliCAT-DARTS: A High Fidelity, Closed-Loop Rotorcraft Simulator for Planetary Exploration.

14. Handling Qualities Assessment and Discussion for Helicopter with Slung Load Systems Utilizing Various Sling Configurations.

15. Radar detectability of light aircraft micro‐Doppler modulation

16. Adaptive fault‐tolerant control of a nonlinear 2‐DOF helicopter system with prescribed performance

19. The high life.

20. HOSTAGES OF CIRCUMSTANCE.

21. EXPANDED CAPABILITIES.

22. Highlights from AirVenture 2024.

23. Farnborough Airshow 2024: Smarter Aviation.

24. Romeo Refreshed.

26. ONE IF BY LAND & TWO IF BY SEA.

27. FIRED UP: An in-depth look at the California Department of Forestry and Fire Protection (CALL FIRE).

28. 基于 Z-5B 型无人直升机的航空物探 (磁/放) 测量技术研究及应用.

29. Micro‐motion signal time‐frequency results inversion of rotor targets under low signal‐to‐noise ratios

30. Oxygen accumulation and associated dangers in rescue helicopters.

31. Hovering performance analysis of helicopter rotor blades using supercritical airfoil.

32. Haiti's 'Sin' of Resistance.

33. Finite-Time Prescribed Performance Tracking Control for Unmanned Helicopter System Using Neural Network.

34. A study on optimal rotor speed control method for helicopter power system considering the influence of infrared suppressors.

35. Conversion of a Coaxial Rotorcraft to a UAV—Lessons Learned †.

36. 直升机传动系统轴承试验机设计.

37. LIFETIME DETERMINATION OF ULTRALIGHT HELICOPTER BLADES.

38. Rotorcraft Flight Control Design for Rotor Noise Abatement.

39. Individual Blade Control for Component Load Alleviation Using Higher-Order Linear Time-Invariant Models.

40. Neural Network Signal Integration from Thermogas-Dynamic Parameter Sensors for Helicopters Turboshaft Engines at Flight Operation Conditions.

41. THE ROYAL AUSTRALIAN SURVEY CORPS' DOPPLER SATELLITE YEARS 1971-1992.

42. Flight dynamics and manipulation strategy of compound high speed helicopter.

43. Unique Operating Conditions Analysis of Turboshaft Engines Based on Nonlinear Integrated Model.

44. Optimization Method for Assembly Sequence Evaluation Based on Assembly Cost and Ontology of Aviation Reducers.

45. A Review on the State of the Art in Copter Drones and Flight Control Systems.

46. Micro‐motion signal time‐frequency results inversion of rotor targets under low signal‐to‐noise ratios.

47. Mixed-Integer MPC for Closed-Loop Motion Planning and Flight Control of a Laboratory Helicopter.

48. An Efficient Analysis Method of Aluminum Alloy Helicopter Fuselage Projectile Damage Based on Projectile Breakdown Theory.

49. Coaxial Helicopter Attitude Control System Design by Advanced Model Predictive Control under Disturbance.

50. Ice Object Exclusion Characteristics of Turboshaft Engine Inlet under Helicopter/Inlet Integration Conditions.

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