This abstract discusses the design, analysis, and construction of a vertical takeoff and landing (VTOL) RC copter (Bliamis et al. 2020). VTOL RC copters combine the benefits of helicopters and fixed-wing aircraft, offering a compact and maneuverable platform for vertical takeoff and landing. The design process involves exploring basic aerodynamic principles and control mechanisms to achieve optimal flight performance. The construction phase involves assembly, testing, and fine-tuning for reliable VTOL capabilities. These aircraft can perform autonomous flight, object tracking, and obstacle avoidance (Hadsanggeni and Nugraha 2015). Designing a VTOL RC copter presents challenges such as balancing weight and performance, addressing stability issues during transitions between vertical and horizontal flight, and transitioning from vertical takeoff to regular aircraft motion. This paper provides a comprehensive overview of the design, analysis, and construction of VTOL RC copters, covering key aspects such as rotor system, frame design, flight controller, and power system. It emphasizes the importance of analyzing and testing the design before flying the VTOL RC copter.