Survey-augmented navigation system for an aircraft
A system having components coupled to an aircraft and components remote from the aircraft processes radar-augmented data, transmits information between aircraft system components and/or remote system components, and dynamically determines locations and states of the aircraft, while the aircraft is in flight. Based on the locations and states of the aircraft, the system generates instructions for flight control of the aircraft toward a flight path appropriate to the locations of the aircraft, and can update flight control instructions as new data is received and processed.
1. A method for radar-augmented localization, the method comprising:
monitoring an altitude status of an aircraft in flight using an altitude sensor while a radar subsystem of the aircraft is in an inactive mode;
in response to the altitude status satisfying a threshold altitude condition, transitioning the radar subsystem of the aircraft from the inactive mode to an active mode of the radar subsystem;
while the radar subsystem is in the active mode, emitting, by the radar subsystem, a radio frequency signal in a radio portion of an electromagnetic spectrum and characterizing an object height of an object below the aircraft based on the radio frequency signal reflected off the object and received by the radar subsystem;
generating a set of candidate locations of the aircraft from the object height; and
determining a location and a state estimate of the aircraft upon processing the set of candidate locations.
2. The method of claim 1 , further comprising: upon detecting availability of a satellite signal from a global positioning system (GPS) of the aircraft, receiving a GPS output from the GPS and determining the location and the state of the aircraft from the set of candidate locations based on the GPS output.
3. The method of claim 1 , further comprising: with the state estimate, the set of candidate locations, and the object height, updating a running index of an aggregation of state estimates mapped to an aggregation of candidate locations and an aggregation of object heights from historical flights of the aircraft.
4. The method of claim 3 , further comprising: upon processing information from the radar subsystem in the active mode, characterizing a second object height of a second object below the aircraft, performing a matching operation with the second object height and the running index, and determining a second location and a second state estimate of the aircraft from the matching operation.
5. The method of claim 3 , wherein the object comprises a static object positioned below the aircraft, and wherein determining the location of the aircraft further comprises applying an iterative solver operation to the object height of the static object and the running index.
6. The method of claim 1 , wherein the object comprises a radar-responsive marker positioned below the aircraft in flight and transitionable into an activated mode upon receiving a radar signal from the radar subsystem, the method further comprising emitting a radar pulse from the radar subsystem, receiving a response signal from the radar-responsive marker in the activated mode, and determining the location and the state estimate from the response signal.
7. The method of claim 1 , wherein the object comprises a dynamic object, and wherein the method further comprises determining the set of candidate locations from a path of motion of the dynamic object and the object height of the dynamic object.
8. The method of claim 7 , wherein the dynamic object comprises a terrestrial vehicle, and wherein determining the set of candidate locations further comprises receiving a set of radar signals returned from the terrestrial vehicle along the path of motion, and determining the set of candidate locations from the set of radar signals.
9. The method of claim 1 , wherein the object comprises a terrain feature positioned below the aircraft.
10. The method of claim 1 , further comprising: based upon at least one of the location and the state estimate, generating a set of instructions for a flight computer of the aircraft, the set of instructions for flight control of the aircraft toward a flight path appropriate for the location.
11. A method for radar-augmented localization, the method comprising:
monitoring an altitude status of an aircraft in flight using an altitude sensor while a radar subsystem of the aircraft is in an inactive mode;
in response to the altitude status satisfying a threshold altitude condition, transitioning the radar subsystem of the aircraft from the inactive mode to an active mode of the radar subsystem;
while the radar system in the active mode, emitting, by the radar subsystem, a radio frequency signal in a radio portion of an electromagnetic spectrum and characterizing an object height of an object below the aircraft based on the radio frequency signal reflected off the object and received by the radar subsystem; and
determining a location and a state estimate of the aircraft from the object height.
12. The method of claim 11 , further comprising: receiving an inertial measurement unit (IMU) output of an IMU coupled to the aircraft and determining the location of the aircraft using the IMU output.
13. The method of claim 11 , further comprising: with the state estimate, the location, and the object height, updating a running index of an aggregation of state estimates mapped to an aggregation of candidate locations and an aggregation of object heights from historical flights of the aircraft.
14. The method of claim 11 , wherein determining the location and the state estimate comprises applying an iterative solver operation to the object height and a running index of an aggregation of state estimates mapped to an aggregation of candidate locations and an aggregation of object heights from historical flights of the aircraft.
15. The method of claim 11 , further comprising: based upon at least one of the location and the state estimate, generating a set of instructions for a flight computer of the aircraft, the set of instructions for flight control of the aircraft toward a flight path appropriate for the location.
16. A system for radar-augmented localization, the system comprising:
a navigation subsystem coupled to an aircraft and comprising a radar subsystem oriented to receive radar signals transmitted toward a ventral portion of the aircraft;
a data transmission subsystem in communication with the navigation subsystem; and
a computing system in communication with the data transmission system and comprising machine-readable instructions in non-transitory media for:
monitoring an altitude status of an aircraft in flight using an altitude sensor while the radar subsystem of the aircraft is in an inactive mode;
in response to the altitude status satisfying a threshold altitude condition, transitioning the radar subsystem of the aircraft from the inactive mode to an active mode of the radar subsystem;
while the radar system is in the active mode, emitting, by the radar subsystem, a radio frequency signal in a radio portion of an electromagnetic spectrum and characterizing an object height of an object below the aircraft based on the radio frequency signal reflected off the object and received by the radar subsystem;
generating a set of candidate locations of the aircraft from the object height; and
determining a location and a state estimate of the aircraft from the object height.
17. The system of claim 16 , wherein the navigation subsystem further comprises an inertial measurement unit (IMU) mounted to the aircraft, and a global positioning system (GPS) coupled to the aircraft, the IMU and the GPS communicatively coupled to the computing system and the radar subsystem.
18. The system of claim 17 , wherein the computing system further comprises instructions for determining the location of the aircraft from processing the set of candidate locations with an IMU output of the IMU and a GPS output of the GPS.
19. The system of claim 16 , wherein the state estimate comprises a position, a velocity, and an orientation of the aircraft.
20. The system of claim 16 , further comprising an electronic interface between the computing system and a flight management system of the aircraft, the electronic interface operable in a mode that transmits the set of instructions to the flight management system and controls flight of the aircraft toward the flight path.