Research Article
Model-Based Design, HIL Testing, and Rapid Control Prototyping of a Low-Cost POC Quadcopter with Stability Analysis and Control
| Symbols | Description |
| | X position w.r.t BFR | | Y position w.r.t BFR | | Z position w.r.t BFR | x | X position w.r.t EFR | Y | Y position w.r.t EFR | Z | Z position w.r.t EFR | | Angular position phi | | Angular position theta | | Angular position psi | | Eta – viscosity | | Rotation matrix | | Rotor inertia | | Diagonal inertia matrix | | Angular rate | | Moment of inertial along the x-axis | | Moment of inertial along the y-axis | | Moment of inertial along the z-axis | | Moment of inertia for body frame principle axes | | Drag coefficients | | Aerodynamic force | | Moment force | | Quadcopter moment | | Drag force | | Moment constant | | Aerodynamic force constant | P | Pitch | | Thrust | D | Diameter | | Required | | Battery voltage | | Nominal | | Output power | | Battery capacity | | Nominal current | | Endurance | | Efficiency |
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