Coordinating spatial and temporal arrival of munitions

A munition navigation system for providing coordination of a munition with a plurality of other munitions in a salvo to form a constellation of munitions in a Global Positioning System (GPS) denied attack of a plurality of ground targets, comprising:

• a datalink communication system configured and operable to communicate with other munitions;
• a seeker component configured and operable for recognizing a ground target;
• a navigation system for navigating the munition in flight, wherein the navigation system is communicatively coupled to the datalink communication system and the seeker component, the navigation system having a memory configured to store instructions a processor disposed in communication with the memory, wherein the processor upon execution of the instructions is configured to:
• determine a relative position of the munition relative to the other munitions in the salvo via the datalink communication system;
• determine a distance range of the munition relative to the other munitions in the salvo via the datalink communication system;
• determine a constellation formation of the plurality of munitions in the salvo based upon the determined relative position and distance range of each munition relative to one another;
• determine a target seeker basket coordinate for the munition in the constellation formation relative to other determined target seeker basket coordinates respectively for other munitions in the salvo relative to the plurality of ground targets;
• and
• navigate the munition to the determined target seeker basket coordinate.

A method for coordination of a plurality of munitions in a salvo to form a constellation of munitions in a Global Positioning System (GPS) denied attack of a plurality of ground targets wherein each munition is provided with a datalink communication system to communicate with other munitions and a navigation system for guiding the munition in flight, the method comprising:

• determining a relative position of each munition relative to the other munitions in the salvo via each munitions' datalink communication system wherein Two-Way Timing and Ranging (TRTW) techniques are utilized by the navigation system of each munition to determine positioning of each munition relative to one another;
• determining a distance range of each munition relative to the other munitions in the salvo via each munitions' datalink communication system;
• determining a constellation formation of the plurality of munitions in the salvo based upon the determined relative position and distance range of each munition relative to one another;
• determining a target seeker basket coordinate respectively for each munition determined to be in the constellation formation relative to the plurality of ground targets;
• and
• navigating each munition in the constellation formation to its respective target seeker basket coordinate via the navigation system of each munition, wherein navigating each munition to its respective target seeker basket coordinate includes coordinating a flight path of each munition in the salvo relative to one another regarding the flight path of each munition to its respective determined target seeker basket, and wherein coordinating a flight path of each munition includes determining an Estimated Time of Arrival (ETA) for each munition relative to its determined target seeker basket.