Geophysical survey system using hybrid aircraft

1. A method for performing a geophysical survey using a hybrid aircraft which includes an apparatus configured to perform the geophysical survey, the method comprising:

transmitting by three mutually orthogonal transmitters electromagnetic (EM) waveforms towards the ground which creates a secondary magnetic field, wherein the three mutually orthogonal transmitters are attached to the hybrid aircraft;

obtaining measurements associated with the secondary magnetic field by three mutually orthogonal null-coupled receivers, wherein the three mutually orthogonal null-coupled receivers are attached to the hybrid aircraft; and

obtaining measurements by three mutually orthogonal gradient receivers, wherein the three mutually orthogonal gradient receivers are attached to the hybrid aircraft.

2. The method of claim 1 , wherein the hybrid aircraft includes a propulsion element and at least one buoyancy element, wherein the at least one buoyancy element contains a lighter than air gas.

3. The method of claim 1 , further comprising:

transmitting at a transmitter pulse repetition frequency of 30 Hz when firing each of the three mutually orthogonal transmitters sequentially.

4. The method of claim 1 , further comprising:

transmitting at a transmitter pulse repetition frequency of 29.5 Hz for a first one the three mutually orthogonal transmitters;

transmitting at a transmitter pulse repetition frequency of 30 Hz for a second one the three mutually orthogonal transmitters; and

transmitting at a transmitter pulse repetition frequency of 31 Hz for a third one the three mutually orthogonal transmitters,

wherein the transmitters are fired non-sequentially.

5. The method of claim 1 , further comprising:

controlling a power level for each axis of the apparatus for steering or sweeping of a primary magnetic field.

6. The method of claim 5 , wherein the power level is the same for each axis of the apparatus.

7. The method of claim 5 , wherein the power level is different for each axis of the apparatus.

8. A system for performing a geophysical survey using a hybrid aircraft which includes an apparatus configured to perform the geophysical survey, the system comprising:

three mutually orthogonal transmitters configured to transmit electromagnetic (EM) waveforms towards the ground which creates a secondary magnetic field, wherein the three mutually orthogonal transmitters are attached to the hybrid aircraft;

three mutually orthogonal null-coupled receivers configured to obtain measurements associated with the secondary magnetic field, wherein the three mutually orthogonal null-coupled receivers are attached to the hybrid aircraft; and

three mutually orthogonal gradient receivers configured to obtain measurements, wherein the three mutually orthogonal gradient receivers are attached to the hybrid aircraft.

9. The system of claim 8 , wherein the hybrid aircraft further comprises:

a propulsion element and at least one buoyancy element, wherein the at least one buoyancy element contains a lighter than air gas.

10. The system of claim 8 , further comprising:

the three mutually orthogonal transmitters configured to transmit at a pulse repetition frequency of 30 Hz when firing each of the three mutually orthogonal transmitters sequentially.

11. The system of claim 8 , further comprising:

a first one of the three mutually orthogonal transmitters configured to transmit at a pulse repetition frequency of 29.5 Hz;

a second one of the three mutually orthogonal transmitters configured to transmit at a pulse repetition frequency of 30 Hz; and

a third one of the three mutually orthogonal transmitters configured to transmit at a transmitter pulse repetition frequency of 31 Hz, wherein the transmitters are fired non-sequentially.

12. The system of claim 8 , wherein a power level for each axis of the apparatus is controllable for steering or sweeping of a primary magnetic field.

13. The system of claim 12 , wherein the power level is the same for each axis of the apparatus.

14. The system of claim 12 , wherein the power level is different for each axis of the apparatus.

15. A system comprising:

a hybrid aircraft;

a three axis geophysical transmitter array, wherein the three axis geophysical array includes a set of three mutually orthogonal electromagnetic transmitters, wherein the transmitters are attached to the hybrid aircraft;

a set of three mutually orthogonal null-coupled receivers, wherein the set of three mutually orthogonal null-coupled receivers are attached to the hybrid aircraft; and

a set of three mutually orthogonal gradient receivers configured to obtain measurements, wherein the set of three mutually orthogonal gradient receivers are attached to the hybrid aircraft.

16. The system of claim 15 , wherein the hybrid aircraft further comprises:

a propulsion element and at least one buoyancy element, wherein the at least one buoyancy element contains a lighter than air gas.

17. The system of claim 15 , further comprising:

the three mutually orthogonal transmitters configured to transmit at a same pulse repetition frequency when firing each of the three mutually orthogonal transmitters sequentially.

18. The system of claim 15 , further comprising:

the three mutually orthogonal transmitters configured to transmit at a different pulse repetition frequency when firing each of the three mutually orthogonal transmitters non-sequentially.

19. The system of claim 15 , wherein a power level for each axis of the three axis geophysical transmitter array is controllable for steering or sweeping of a primary magnetic field.