System and methods for battery management and control of an electric vehicle

A computer-readable medium storing instructions that, when executed by at least one processor, cause the at least one processor to:

• receive electrical information of one or more batteries measured using a first sensor;
• estimate an aircraft-level energy based on the electrical information of the one or more batteries;
• receive an altitude of the aircraft and a current airspeed of the aircraft measured using a second sensor;
• estimate a steady-state force based on the altitude of the aircraft and the current airspeed of the aircraft;
• estimate a vertical landing range and a horizontal landing range based on the estimated aircraft-level energy and the estimated steady-state force;
• and
• display the estimated vertical landing range and the estimated horizontal landing range on a display.

A system, comprising:

• at least one processor;
• and
• at least one computer-readable medium containing instructions that, when executed by the at least one processor, cause the at least one processor to;
• receive electrical information of one or more batteries measured using a first sensor;
• estimate an aircraft-level energy based on the electrical information of the one or more batteries;
• receive an altitude of the aircraft and a current airspeed of the aircraft measured using a second sensor;
• estimate a steady-state force based on the altitude of the aircraft and the current airspeed of the aircraft;
• estimate a vertical landing range and a horizontal landing range based on the estimated aircraft-level energy and the estimated steady-state force;
• and
• display the estimated vertical landing range and the estimated horizontal landing range on a display.

An aircraft, comprising:

• at least one processor;
• and
• at least one computer-readable medium containing instructions that, when executed by the at least one processor, cause the at least one processor to:
• receive electrical information of one or more batteries measured using a first sensor;
• estimate an aircraft-level energy based on the electrical information of the one or more batteries;
• receive an altitude of the aircraft and a current airspeed of the aircraft measured using a second sensor;
• estimate a steady-state force based on the altitude of the aircraft and the current airspeed of the aircraft;
• estimate a vertical landing range and a horizontal landing range based on the estimated aircraft-level energy and the estimated steady-state force;
• and
• display the estimated vertical landing range and the estimated horizontal landing range on a display.