Adaptive airdrop system and method
An adaptive airdrop system for an aircraft includes a wind measurement system and a processing system. The wind measurement system measures at least atmospheric wind velocity and supplies wind velocity data representative thereof. The processing system is configured to adaptively sample the wind velocity data, implement a computer aided release point (CARP) model, and iteratively process the adaptively sampled wind velocity data to calculate, using the CARP model, a precision release point for a payload.
1. An adaptive airdrop system for an aircraft flying at a cruising altitude above ground, comprising:
a wind measurement system configured to measure at least atmospheric wind velocity at a plurality of different altitudes from the ground to the cruising altitude of the aircraft and supply wind velocity data representative thereof;
a processing system in operable communication with the wind measurement system and configured to:
(i) adaptively sample the wind velocity data,
(ii) implement a computer aided release point (CARP) model, and
(iii) iteratively process the adaptively sampled wind velocity data to calculate, using the CARP model, a precision release point for a payload and a projected trajectory of the payload if it is released from the precision release point;
and
a flight management system (FMS) in operable communication with the processing system, the FMS configured to implement a flight plan, and further configured to:
(i) receive data representative of the precision release point for the payload,
(ii) update the flight plan to reflect the precision release point, and
(iii) guide the aircraft along the updated flight plan,
wherein the wind measurement system is further configured to:
receive data representative of the projected trajectory of the payload from the processing system;
measure at least the atmospheric wind velocity at different altitudes along the projected trajectory of the payload; and
supply updated wind velocity data.
2. The system of claim 1 , further comprising:
a display device in operable communication with the processing system, the display device configured to at least selectively display the precision release point.
3. The system of claim 1 , wherein the wind measurement system comprises an ultraviolet LIDAR (UV LIDAR) system.
4. The system of claim 1 , wherein the wind measurement system is further configured to measure one or more of temperature, density, pressure, and humidity.
5. An adaptive airdrop system for an aircraft flying at a cruising altitude above ground, comprising:
an ultraviolet LIDAR (UV LIDAR) system configured to measure one or more atmospheric conditions at a plurality of altitudes from the ground to the cruising altitude of the aircraft and supply atmospheric condition data representative thereof;
a processing system in operable communication with the UV LIDAR system and configured to:
(i) adaptively sample the atmospheric condition data,
(ii) implement a computer aided release point (CARP) model, and
(iii) iteratively process the adaptively sampled atmospheric condition data to calculate, using the CARP model, a precision release point for a payload and a projected trajectory of the payload if it is released from the precision release point;
and
a flight management system (FMS) in operable communication with the processing system, the FMS configured to implement a flight plan, and further configured to:
(i) receive data representative of the precision release point for the payload,
(ii) update the flight plan to reflect the precision release point, and
(iii) guide the aircraft along the updated flight plan,
wherein the UV LIDAR system is further configured to:
receive data representative of the projected trajectory of the payload from the processing system;
measure at least the atmospheric wind velocity at different altitudes along the projected trajectory of the payload; and
supply updated wind velocity data.
6. The system of claim 5 , further comprising:
a display device in operable communication with the processing system, the display device configured to at least selectively display the precision release point.
7. The system of claim 5 , wherein the one or more atmospheric conditions include wind velocity, temperature, density, pressure, and humidity.
8. An aircraft configured to fly at a cruising altitude above ground, comprising:
a fuselage adapted to have a payload disposed therein; and
a precision airdrop system disposed within the fuselage, the precision airdrop system comprising:
a wind measurement system configured to measure at least atmospheric wind velocity at a plurality of altitudes from the ground to the cruising altitude of the aircraft and supply wind velocity data representative thereof;
a processing system in operable communication with the wind measurement system and configured to:
(i) adaptively sample the wind velocity data,
(ii) implement a computer aided release point (CARP) model,
and
(iii) iteratively process the adaptively sampled wind velocity data to calculate, using the CARP model, a precision release point for the payload and a projected trajectory of the payload if it is released from the precision release point;
and
a flight management system (FMS) in operable communication with the processing system, the FMS configured to implement a flight plan, and further configured to:
(i) receive data representative of the precision release point for the payload,
(ii) update the flight plan to reflect the precision release point,
and
(iii) guide the aircraft along the updated flight plan,
wherein the wind measurement system is further configured to:
receive data representative of the projected trajectory of the payload from the processing system;
measure at least the atmospheric wind velocity at different altitudes along the projected trajectory of the payload; and
supply updated wind velocity data.
9. The aircraft of claim 8 , further comprising:
a display device disposed within the fuselage and in operable communication with the processing system, the display device configured to at least selectively display the precision release point.
10. The aircraft of claim 8 , wherein the wind measurement system comprises an ultraviolet LIDAR (UV LIDAR) system.
11. The aircraft of claim 8 , wherein the wind measurement system is further configured to measure one or more of temperature, density, pressure, and humidity.