A guidance measurement and control system for projectiles, munitions, or rounds released, fired, or deployed from an unmanned aerial vehicle (UAV) comprising:
- at least one projectile, munition, or round adapted to be released, fired, or deployed from a UAV, the at least one project, munition, or round comprising:
- 1. At least one electronics board, the electronics board comprising an upper surface, and a lower surface,
- 2. A plurality of inertial measurement units (IMUs) mounted on at least one of the surfaces of the at least one electronics board, arranged to have both spatial and temporal diversity with respect to other the IMUs for measurement redundancy and error correction, each IMU having a signal measuring at least spin rate, pitch, and roll of the projectile, munition, or round, the IMUs adapted to be interconnected at least via firmware,
- 3. at least one control system adapted to adjust a course of the projectile, munition, or round, and
- 4. at least one actuator adapted to adjust the at least one control system to adjust a course of the projectile, munition, or round;
- a processor adapted to receive the signal from each IMU;
- and
- a guidance algorithm comprised in the processor, the guidance algorithm adapted to:
- 1. Synchronize the signals from each of the IMUs,
- 2. provide a guidance metric representative of an absolute or relative location of the projectile, munition, or round based on the signals of each of the IMUs, and
- 3. provide guidance commands to the at least one actuator to adjust the at least one control system to maneuver the projectile, munition, or round along an adjusted course,
- wherein the guidance commands are based at least in part on the measured spin rate, pitch, and roll of the projectile, munition, or round.