VTOL aircraft having multifocal landing sensors
An aircraft includes an airframe with a thrust array attached thereto. The thrust array includes a plurality of propulsion assemblies that are independently controlled by a flight control system. A landing gear assembly is coupled to the airframe and includes a plurality of landing feet. An altitude sensor array includes a plurality of altitude sensors each of which is disposed within one of the landing feet such that when the aircraft is in the VTOL orientation, the altitude sensor array is configured to obtain multifocal altitude data relative to a landing surface. The flight control system is configured to generate a three-dimensional terrain map of the surface based upon the multifocal altitude data.
1. An aircraft having a VTOL orientation, the aircraft comprising:
an airframe;
a thrust array attached to the airframe, the thrust array including a plurality of propulsion assemblies;
a flight control system coupled to the airframe and operable to independently control each of the propulsion assemblies;
a landing gear assembly coupled to the airframe, the landing gear assembly including a plurality of landing feet; and
an altitude sensor array including a plurality of altitude sensors each disposed within one of the landing feet such that when the aircraft is in the VTOL orientation, the altitude sensor array is configured to obtain multifocal altitude data relative to a surface;
wherein, the flight control system is configured to generate a three-dimensional terrain map of the surface based upon the multifocal altitude data; and
wherein, the flight control system is configured to autonomously orient the aircraft in a preferred landing orientation relative to the surface based upon the three-dimensional terrain map.
2. The aircraft as recited in claim 1 wherein the altitude sensors further comprise radar altimeters configured to reflect radio waves off the surface.
3. The aircraft as recited in claim 1 wherein the altitude sensor array includes at least three altitude sensors.
4. The aircraft as recited in claim 1 wherein the altitude sensor array includes four altitude sensors.
5. The aircraft as recited in claim 1 wherein each of the altitude sensors is disposed proximate a distal end of the respective one of the landing feet.
6. The aircraft as recited in claim 1 wherein the flight control system is configured to determine whether one or more of the landing feet are in contact with the surface based upon the multifocal altitude data.
7. The aircraft as recited in claim 1 wherein the flight control system is configured to identify a suitable landing site based upon the three-dimensional terrain map.
8. The aircraft as recited in claim 1 wherein the flight control system is configured to autonomously orient the aircraft in a preferred landing orientation relative to a slope of the surface based upon the three-dimensional terrain map.
9. The aircraft as recited in claim 1 wherein the flight control system is configured to autonomously orient a lateral axis of the aircraft to be substantially parallel to a slope of the surface prior to the aircraft making a four point landing on the surface.
10. The aircraft as recited in claim 1 wherein the flight control system is configured to autonomously maintain a level flight attitude prior to the aircraft making a two point by two point landing on a portion of the surface having a slope.
11. The aircraft as recited in claim 1 wherein the airframe further comprises first and second wings with first and second pylons extending therebetween;
wherein the thrust array further comprises a two-dimensional distributed thrust array; and
wherein the plurality of propulsion assemblies includes at least two propulsion assemblies coupled to the first wing and at least two propulsion assemblies coupled to the second wing.
12. The aircraft as recited in claim 1 wherein the propulsion assemblies further comprise thrust vectoring propulsion assemblies.
13. A method of operating an aircraft, the method comprising:
locating the aircraft in a VTOL orientation over a surface, the aircraft including an airframe, a plurality of propulsion assemblies coupled to the airframe, a landing gear assembly coupled to the airframe and including a plurality of landing feet each having an altitude sensor disposed therein and a flight control system in communication with the altitude sensors and operable to control the propulsion assemblies;
obtaining multifocal altitude data from the altitude sensors;
generating a three-dimensional terrain map of the surface with the flight control system based upon the multifocal altitude data; and
autonomously orienting the aircraft in a preferred landing orientation relative to the surface based upon the three-dimensional terrain map.
14. The method as recited in claim 13 further comprising identifying a suitable landing site based upon the three-dimensional terrain map.
15. The method as recited in claim 13 further comprising autonomously orienting the aircraft in a preferred landing orientation relative to a slope of the surface based upon the three-dimensional terrain map.
16. The method as recited in claim 13 further comprising autonomously orienting a lateral axis of the aircraft to be substantially parallel to a slope of the surface prior to making a four point landing on the surface.
17. The method as recited in claim 13 further comprising autonomously maintaining a substantially level flight attitude prior to making a two point by two point landing on a portion of the surface having a slope.
18. The method as recited in claim 13 further comprising determining whether one or more of the landing feet are in contact with the surface based upon the multifocal altitude data.