Integrated and modular suspended load control apparatuses, systems, and methods
Load control apparatuses, systems and methods to control a location, orientation, or rotation of a suspended load by imparting thrust vectors to the suspended load or to a structure that holds the load. The load control apparatuses, systems and method may be integrated into a structure that holds a load, such as a rescue litter. The load control apparatuses, systems, and methods may be modular. The modular load control apparatuses, systems, and methods may be secured to a load or to a structure that holds the load.
1. A modular load control system to influence at least one of a position, orientation, or motion of a load suspended by a cable from a carrier, comprising:
a plurality of modular thruster housings, a sensor suite, and a computer processor and memory, wherein the memory comprises a thrust control module which, when executed by the computer processor, is to determine a position, orientation, or motion based on a sensor data from the sensor suite and is to control a plurality of fans in the plurality of thrusters housings according to the position, orientation, or motion to influence at least one of the position, orientation, or motion of the load, further comprising a fan repositioning mechanism, wherein the fan repositioning mechanism allows at least two of the modular thruster housings to be repositioned in the modular load control system.
2. The modular load control system according to claim 1 , wherein to determine the position, orientation, or motion based on the sensor data from the sensor suite comprises to fuse the sensor data from the sensor suite in a non-linear filter to determine a current state of the modular load control system.
3. The modular load control system according to claim 2 , wherein the non-linear filter comprises a non-linear flavor of a Kalman filter.
4. The modular load control system according to claim 2 , wherein the thrust control module is further to project near-term future motion based on the current state.
5. The modular load control system according to claim 4 , wherein to project near-term future motion based on the current state comprises to fuse the sensor data in a non-linear flavor of a Kalman filter.
6. The modular load control system according to claim 2 , wherein to control the plurality of thrusters according to the position, orientation, or motion to influence at least one of the position, orientation, or motion of the load comprises to fuse the sensor data from the sensor suite in the non-linear filter to determine the current state of the modular load control system with feedback from at least one of a functional mode or command state of an operational module, a thrust and orientation mapping, or a fan mapping.
7. The modular load control system according to claim 4 , wherein the control module is further to determine the thrust and orientation mapping according to at least one of an orientation of a fan in plurality of thruster housings or a power signal to the fan in the plurality of thruster housings.
8. A method to influence at least one of a position, orientation, or motion of a load suspended by a cable from a carrier, comprising:
securing a modular thruster housing to the load;
with a computer processor and memory, wherein the memory comprises a thrust control module, performing the thrust control module with the computer processor and thereby determining the position, orientation, or motion of the load based on a sensor data from a sensor suite; and controlling a thruster in the modular thruster housing according to the position, orientation, or motion to influence at least one of the position, orientation, or motion of the load, and further comprising repositioning the modular thruster housing with a fan unit repositioning mechanism.
9. The method according to claim 8 , wherein determining the position, orientation, or motion based on the sensor data from the sensor suite comprises fusing the sensor data from the sensor suite in a non-linear filter to determine a current state of the load.
10. The method according to claim 9 , wherein the non-linear filter comprises a non-linear flavor of a Kalman filter.
11. An apparatus to influence at least one of a position, orientation, or motion of a load suspended by a cable from a carrier, comprising:
means to secure a modular thruster housing to the load;
means to, with a thrust control module in a computer memory, perform the thrust control module and means to thereby determine the position, orientation, or motion of the load based on a sensor data from a sensor suite; and
means to control a thruster in the modular thruster housing according to the position, orientation, or motion to influence at least one of the position, orientation, or motion of the load; and further comprising
means to reposition the modular thruster housing with a fan unit repositioning mechanism.
12. The apparatus according to claim 11 , wherein means to determine the position, orientation, or motion based on the sensor data from the sensor suite comprises means to fuse the sensor data from the sensor suite in a non-linear filter to determine a current state of the load.
13. The apparatus according to claim 12 , wherein the non-linear filter comprises a non-linear flavor of a Kalman filter.
14. The apparatus according to claim 12 , further comprising means to project near-term future motion based on the current state.
15. The apparatus according to claim 12 , wherein means to project near-term future motion based on the current state comprises to means to fuse the sensor data in a non-linear flavor of a Kalman filter.
16. The apparatus according to claim 12 , wherein means to control the plurality of thrusters according to the position, orientation, or motion to influence at least one of the position, orientation, or motion of the load comprises means to fuse the sensor data from the sensor suite in the non-linear filter to determine the current state of the modular load control system with feedback from at least one of a functional mode or command state of an operational module, a thrust and orientation mapping, or a fan mapping.
17. The apparatus according to claim 16 , further comprising mean to determine the thrust and orientation mapping according to at least one of an orientation of a fan in plurality of thruster housings or a power signal to the fan in the plurality of thruster housings.