Systems, methods, and devices for operation of a vehicle

An aircraft control system, comprising:

• a first input device and a second input device, wherein each of the first input device and the second input device is configured to be manipulated by a user, the first input device and the second input device each having a first orientation and a second orientation different from the first orientation;
• at least one rotor operatively connected with a body of an aircraft;
• at least one control surface operatively connected to the body of the aircraft;
• a controller electrically coupled with the first input device, the second input device, the at least one rotor, and the at least one control surface, wherein the controller is configured to:
• determine a speed profile of the aircraft based on a speed of the aircraft;
• determine an orientation of the first input device;
• determine an orientation of the second input device;
• send a command to the at least one rotor and/or the at least one control surface based on the speed profile and the orientation of the first input device and the orientation of the second input device;
• and
• adjust the at least one rotor and/or the at least one control surface.