capabilities and a well-conceived approach. This
paves the way for subsequent analysis and decision-
making, enabling the extraction of valuable
information and precise control over the drone's
movements. The process is showcased through
figures depicting the signal behavior when the
transceiver is turned on and off, as well as how the
signal alters with adjustments to the throttle on the
controller. Such analysis is crucial for ensuring
optimal performance and identifying any potential
issues with the control system.
2 QUADCOPTER
CONSTRUCTION AND
PROBLEM FORMULATION
Quadcopters, a prominent type of UAVs, have
captured researchers' interest due to their exceptional
features. These include high maneuverability,
reliability, versatile applications, and cost-
effectiveness. With their four rotors arranged
symmetrically, quadcopters excel in navigating
complex environments with precision. Their compact
size and straightforward design make them ideal for
various tasks such as aerial photography,
surveillance, search and rescue missions, and package
delivery. This versatility and efficiency make
quadcopters a compelling choice for both research
and practical applications (Ozbek, Onkol, Garcia,
2018).
Various studies explore advancements in
autonomous drone technology. One study introduces
an optimization framework for vision-based
autonomous drone navigation, enhancing tasks like
surveillance and environmental monitoring (Navardi,
Shiri, et al. , 2016). Another research effort focuses
on autonomous drone delivery systems, potentially
revolutionizing last-mile logistics (Kannan;, Min,
Hong, 2019). A separate study discusses continuous
maneuver control and data capture scheduling of
autonomous drones in wireless sensor networks,
aiming to optimize data acquisition efficiency(Li, Ni,
Hong, 2019). Additionally, a proposed resource-
efficient online target detection system utilizes
autonomous drones, enhancing IoT applications
(Wang, Gu, et al. , 2020). Furthermore, research
examines the stability of small-scale UAVs under
PID control with added payload mass, contributing to
the understanding of drone stability (Pounds, Bersak,
et al. , 2019). Another study discusses resilient
control design for intelligent vehicle lateral motion
regulation, offering insights applicable to drone
control systems (Chang, Liu, et al. , 2017). Finally,
visual servoing techniques for micro quadrotors
landing on ground platforms are explored, addressing
challenges in drone precision landing (Huang,
Chiang, et al. , 2022).
In this section of the paper, the investigation into
autonomous drone control methods delved into the
integration of microcontroller-based signal mimicry.
Various aspects of autonomous drones were
explored, focusing on Raspberry Pi Zero and other
inexpensive components. The findings cover real-
world performance, adaptability, ethical
considerations, and the unique contributions of
autonomous drone systems.
In this section, the construction of the drone for
experimentation and reading the signals created by
the transceiver for recreation will be briefly
discussed.
2.1 Drone Construction
In this Subsection, Figure 1 depicts the conventional
quadcopter configuration, comprising four rotors
mounted on arms extending from a central body. Each
rotor is powered by a brushless DC (BLDC) motor,
generating downward thrust forces to achieve vertical
lift. The magnitude and direction of the thrust forces
are adjustable by varying the motor speeds.
Figure 1: Quadcopter Configuration
The drone system employed for our
experimentation utilized cost-effective components
to minimize expenses. The motors were 1000
RPM/Volt BLDC motors, known for their high power
and efficiency. To control the motor speeds, four
electronic speed controllers (ESCs) were utilized.
The drone frame was an f450 model, commonly
preferred by DIY drone builders. Plastic propellers