This thesis documents the research undertaken to develop a high-performing design
of a small-scale quadrotor (four-rotor) helicopter capable of delivering the speed and
robustness required for agile motion while also featuring an autonomous visual servoing
capability within the size, weight, and power (SWaP) constraint package. The
state of the art research was reviewed, and the areas in the existing design methodologies
that can potentially be improved were identified, which included development
of a comprehensive dynamics model of quadrotor, design and construction of a performance
optimized prototype vehicle, high-performance actuator design, design of a
robust attitude stabilization controller, and a single chip solution for autonomous vision
based position control. The gaps in the current art of designing each component
were addressed individually. The outcomes of the corresponding development activities
include a high-fidelity dynamics and control model of the vehicle. The model
was developed using multi-body bond graph modeling approach to incorporate the
dynamic interactions between the frame body and propulsion system. Using an algorithmic
size, payload capacity, and flight endurance optimization approach, a quadrotor
prototype was designed and constructed. In order to conform to the optimized
geometric and performance parameters, the frame of the prototype was constructed
using printed circuit board (PCB) technology and processing power was integrated
using a single chip field programmable gate array (FPGA) technology. Furthermore, to actuate the quadrotor at a high update rate while also improving the power efficiency
of the actuation system, a ground up FPGA based brushless direct current
(BLDC) motor driver was designed using a low-loss commutation scheme and hall
effect sensors. A proportional-integral-derivative (PID) technology based closed loop
motor speed controller was also implemented in the same FPGA hardware for precise
speed control of the motors. In addition, a novel control law was formulated for robust
attitude stabilization by adopting a cascaded architecture of active disturbance rejection
control (ADRC) technology and PID control technology. Using the same single
FPGA chip to drive an on-board downward looking camera, a monocular visual servoing
solution was developed to integrate an autonomous position control feature with
the quadrotor. Accordingly, a numerically simple relative position estimation technique
was implemented in FPGA hardware that relies on a passive landmark/target
for 3-D position estimation.
The functionality and effectiveness of the synthesized design were evaluated by
performance benchmarking experiments conducted on each individual component as
well as on the complete system constructed from these components. It was observed
that the proposed small-scale quadrotor, even though just 43 cm in diameter, can lift
434 gm of payload while operating for 18 min. Among the ground up designed components,
the FPGA based motor driver demonstrated a maximum of 4% improvement in
the power consumption and at the same time can handle a command update at a rate
of 16 kHz. The cascaded attitude stabilization controller can asymptotically stabilize
the vehicle within 426 ms of the command update. Robust control performance under
stochastic wind gusts is also observed from the stabilization controller. Finally, the
single chip FPGA based monocular visual servoing solution can estimate pose information
at the camera rate of 37 fps and accordingly the quadrotor can autonomously
climb/descend and/or hover over a passive target