Method and system for increasing safety in chemical application from an aircraft
This invention relates to a method and system for increasing safety in chemical application from an aircraft. Wind speed, wind direction and other critical flight parameters are measured, calculated, recorded, and visually or audibly announced during the aircraft flight via onboard equipment, which parameters provide a means for the aircraft pilot to control chemical spray application and for unassisted automatic chemical spray cutoff and for limiting spray application outside an application zone or target area. Such parameters also provide a means for indicating the lift reserve of the aircraft and a means for determining atmospheric stability near the ground and providing the pilot with a record of the meteorological conditions at a particular location. The method and system of the present invention also provide a means for predicting appropriate aircraft upwind offset distance to compensate for predicted chemical spray drift.
1. A method for computing wind speed and wind direction from an aircraft, the method comprising:
means for measuring airspeed of the aircraft;
means for measuring barometric pressure;
means for determining bearing of the aircraft;
means for determining ground speed of the aircraft;
means for determining a first wind velocity component in the direction of a first pair of flight passes;
means for determining a second wind velocity component in the direction of a second pair of flight passes;
means for correcting a wind velocity component to true north and perpendicular axis; and
processing means for computing wind speed and wind direction.
2. The method according to claim 1 , wherein the aircraft delivers chemicals to an application zone.
3. The method according to claim 2 , wherein the application zone comprises a target area selected from a group consisting of a row crop field, forest, fruit tree orchard, urban area, non-urban area, non-row crop area, pasture, swamp, and marsh.
4. The method according to claim 1 , wherein the means for measuring airspeed comprises:
a pitot tube including a port for measuring static and dynamic air pressure;
a static port included on said pitot tube for measuring static air pressure only;
a first differential pressure transducer including a sensor for measuring dynamic pressure; and
a barometric pressure sensor.
5. The method according to claim 1 , wherein the means for determining bearing of the aircraft comprises a global positioning system.
6. The method according to claim 1 , wherein the means for determining ground speed of the aircraft comprises a global positioning system.
7. The method according to claim 1 , wherein the processing means for computing wind speed and wind direction comprises:
means for recording wind speed and wind direction at flight height;
at least one analog to digital converter;
an onboard processor; and
an onboard computer.
8. The method according to claim 1 , wherein the processing means for computing wind speed and wind direction further comprises:
at least one illuminated switch for visual annunciation of status of functions;
a touch screen; and
a voice playback module for receiving signals for audio playback and providing audio playback signals to the aircraft audio system.
9. The method according to claim 7 , wherein the onboard processor comprises an application specific integrated circuit (ASIC), a microcontroller, a computer system, a processor, a microprocessor, a digital signal processor (DSP), or combinations thereof.
10. The method according to claim 7 , wherein the onboard computer comprises a processor, microprocessor, or combination thereof.