Expandable Fully Actuated Aerial Vehicle Assembly: Geometric Control Adapted from an Existing Flight Controller and Real-World Prototype Implementation

Engineering

• Spherical Joint 100%
• Design Procedure 50%
• Fits and Tolerances 50%
• Similarities 50%
• Degree of Freedom 50%
• Systems Dynamics 50%
• Controller Design 50%
• Payload Capacity 50%
• Control Design 50%
• Configuration Space 50%
• Design Criterion 50%
• Communication Protocol 50%