IP Library Granted Patent US 11,619,470
Granted Patent B2
US 11,619,470 · App. 17/099,592 · Granted Apr 4, 2023

Systems and methods of calculating a ballistic solution for a projectile

Inventor: Daniel Baumgartner (Beverly Hills, CA)
Assignee: Knightwerx Inc.
F41G3/08B64C39/024B64U2101/15
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Quick Facts
Patent No.
US 11,619,470
App. No.
17/099,592
Granted
Apr 4, 2023
Kind
B2
Abstract

Systems and methods of calculating a ballistic solution for a projectile are provided. A ballistic system may include an airborne device, a ballistic computer, a data interface, and a flight module, or any combination thereof. The airborne device (e.g., a drone) may be operable to gather wind data along or adjacent to a flight path of a projectile to a target. The ballistic computer may be in data communication with the airborne device to receive the wind data. The ballistic computer may be configured to calculate a ballistic solution for the projectile based on the wind data. The data interface may be in data communication with the ballistic computer to output the ballistic solution to a user. The flight module may be configured to calibrate a flight path of the airborne device.

Claims (49)

1. A ballistic system comprising:

an airborne device configured to gather wind data along a flight path of a projectile to a target;

a ballistic computer configured to calculate a ballistic solution for the projectile based on the wind data;

a controller configured to designate a location to place the airborne device along the flight path of the projectile; and

a processor configured to determine a flight path of the airborne device to the location.

2. The ballistic system of claim 1 , wherein the controller is mountable on a weapons system.

3. The ballistic system of claim 1 , wherein the controller is configured to designate the location based on a characteristic of a weapons system or one or more target characteristics.

4. The ballistic system of claim 3 , wherein the characteristic comprises at least one of a slant angle of the weapons system, a range to the target, or a direction of fire of the weapons system relative to at least the geo-location of a shooter and the target.

5. The ballistic system of claim 1 , wherein the airborne device is configured to be:

auto-piloted from a mission control system or a shooter to a designated position; and

auto-piloted back to the mission control system or the shooter.

6. The ballistic system of claim 1 , wherein:

the airborne device is configured to execute automated landing procedures at a designated position; and

the airborne device further comprises a wind sensor configuration operable to collect data at the designated position.

7. The ballistic system of claim 1 , wherein the airborne device is configured to place a wind sensor at a designated position.

8. The ballistic system of claim 1 , wherein the flight path of the airborne device comprises different elevations of the airborne device based on a mode of the ballistic system.

9. The ballistic system of claim 8 , wherein:

a first mode of the ballistic system hovers the airborne device above a trajectory elevation of the projectile to the target;

a second mode of the ballistic system hovers the airborne device at the trajectory elevation of the projectile to the target; and

a third mode of the ballistic system places the airborne device below the trajectory elevation of the projectile to the target.

10. The ballistic system of claim 1 , wherein:

the airborne device is configured to detect a threat to the airborne device or the wellbeing of a user; and

detection of the threat or the wellbeing of the user triggers a notification to the user, an altitude adjustment of a hover position of the airborne device, or a relocation maneuver of the airborne device.

11. The ballistic system of claim 1 , further comprising:

a plurality of airborne devices, wherein each airborne device is configured to gather wind data in respective ballistic segments of the flight path of the projectile;

wherein the controller is configured to designate a plurality of locations to place the plurality of airborne devices along the flight path of the projectile; and

wherein the processor is configured to determine respective flight paths for the plurality of airborne devices to the plurality of locations.

12. The ballistic system of claim 1 , wherein the airborne device further comprises a wind sensor configuration operable to collect data after landing at a designated location.

13. A ballistic system comprising:

at least one airborne device operable to gather wind data along a flight path of a projectile to a target; and

one or more processors configured to execute instructions that cause the ballistic system to perform operations comprising:

designating a location to place the at least one airborne device along the flight path of the projectile

determining a flight path of the at least one airborne device to the location;

receiving the wind data from the at least one airborne device; and

calculating a ballistic solution for the projectile based at least partially on the wind data.

14. The ballistic system of claim 13 , wherein the location is designated based on at least one of a slant angle of a weapons system, a range to the target, or a direction of fire of the weapons system relative to at least the geo-location of a shooter and the target.

15. The ballistic system of claim 13 , further comprising a wind sensor configured to be carried by the airborne device to a designated position, wherein the operations further comprise receiving wind data from the wind sensor, and wherein the ballistic solution is calculated based on the wind data received from the wind sensor.

16. The ballistic system of claim 13 , wherein the operations further comprise determining an elevation of the at least one airborne device based on a mode of the ballistic system.

17. The ballistic system of claim 13 , wherein the operations further comprise adjusting a position of the at least one airborne device in response to a detection of a threat to the at least one airborne device or the wellbeing of a user.

18. The ballistic system of claim 13 , wherein:

the at least one airborne device comprises a plurality of airborne devices configured to gather wind data in respective ballistic segments of the flight path of the projectile;

the designating the location comprises designating a plurality of locations to place the plurality of airborne devices along the flight path of the projectile; and

the determining the flight path comprises determining respective flight paths for the plurality of airborne devices to the plurality of locations.

19. The ballistic system of claim 13 , wherein the determining the flight path comprises at least one of:

determining a path that limits at least one of an identification of the at least one airborne device in flight or a tracking of the at least one airborne device back to a shooting position; or

programming the at least one airborne device to fly in a random flight pattern.

20. The ballistic system of claim 13 , wherein the operations further comprise:

landing the at least one airborne device at a designated position; and

collecting wind data from the at least one airborne device at the designated position.

Assignments (3)
NUNC PRO TUNC ASSIGNMENT Recorded Oct 10, 2022
From: BAUMGARTNER, DANIEL
To: KNIGHTWERX INC.
Reel/Frame 061361/0378 →
CHANGE OF NAME Recorded Aug 12, 2022
From: MOONWERX INC.
To: KNIGHTWERX INC.
Reel/Frame 061133/0200 →
CHANGE OF NAME Recorded Aug 12, 2022
From: ARMADA AEROSPACE INC.
To: MOONWERX INC.
Reel/Frame 061200/0497 →
Continuity (3)
Continuation 16822925 · Mar 18, 2020
Provisional Application 62820017 · Mar 18, 2019
Related Publication 20210254932A1 · Aug 19, 2021
Cited By (1)
US 12,242,284