公开(公告)号：US20240343416A1

公开(公告)日：2024-10-17

申请号：US18633447

申请日：2024-04-11

Applicant: ASTROBOTIC TECHNOLOGY, INC.

Inventor： CEDRIC CORPA DE LA FUENTE ,  TROY ARBUCKLE ,  KERRY QUINN ,  ANDREA DAVIS ,  MIKE PROVENZANO ,  JOSEPH ZIMO ,  UPASANA LNU ,  JOSHUA SHAPIRO ,  NOAH GASPARRO

IPC: B64G1/16 ,  B64G1/40 ,  B64G1/42 ,  B64G1/66

CPC classification number: B64G1/16 ,  B64G1/411 ,  B64G1/425 ,  B64G1/66

Abstract: A spacecraft includes a body having a motor, a lander interface, a sensor and a power source for powering the motor and the sensor, and the power source being mounted thereon. An integrated avionics unit has a module and an integrated circuit with the module having a central computer and a motor controller for controlling the motor and the integrated circuit having a temperature monitoring system for monitoring the temperature of the spacecraft and a power regulator having a cell balancer for regulating the power of the power source. The module and the integrated circuit are connected to one another for constant communication therebetween. The central computer communicates with the sensor.