Systems, devices, and/or methods for managing targeted payload descent
First Claim
Patent Images
1. A device comprising:
- a substantially cylindrical sonobuoy glide harness adapted to;
be operably connected to a substantially cylindrical sonobuoy internal module to form a sonobuoy vehicle, the sonobuoy vehicle adapted to launch from a sonobuoy launch container that defines a sonobuoy launch container inner diameter, the sonobuoy vehicle defining a sonobuoy vehicle length and a sonobuoy vehicle outer diameter; and
operatively replace a substantially cylindrical external housing that is operatively adapted to substantially surround the sonobuoy internal module, the external housing defining an external housing length and an external housing outer diameter, the sonobuoy vehicle length not exceeding the external housing length, the sonobuoy vehicle outer diameter not exceeding the sonobuoy launch container inner diameter;
the sonobuoy glide harness comprising;
a stabilization parachute adapted to provide stabilization of the sonobuoy vehicle while the sonobuoy vehicle is in flight;
a stabilization parachute ejection mechanism adapted to, while the sonobuoy vehicle is in flight, release the stabilization parachute from the sonobuoy vehicle;
a plurality of deployable aerodynamic control surfaces;
an actuation system operatively adapted to deploy the plurality of deployable aerodynamic control surfaces during and/or after launch of the sonobuoy vehicle from a flying aircraft;
a guidance system operatively adapted to provide a dynamically determined, substantially controlled, and substantially guided descent of the sonobuoy vehicle from a release altitude, latitude, and longitude located within a predetermined release zone and toward a predetermined sonobuoy water entry zone that is defined by a predetermined range of water entry longitudes and a predetermined range of water entry latitudes; and
an aerodynamic control surface ejection mechanism adapted to substantially simultaneously release the aerodynamic control surfaces from the sonobuoy vehicle and deploy a terminal parachute.
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Abstract
Certain exemplary embodiments can provide a system, machine, device, manufacture, circuit, composition of matter, and/or user interface adapted for and/or resulting from, and/or a method and/or machine-readable medium comprising machine-implementable instructions for, activities that can comprise and/or relate to, providing a guided descent from a release zone and toward an entry zone.
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Citations
24 Claims
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1. A device comprising:
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a substantially cylindrical sonobuoy glide harness adapted to; be operably connected to a substantially cylindrical sonobuoy internal module to form a sonobuoy vehicle, the sonobuoy vehicle adapted to launch from a sonobuoy launch container that defines a sonobuoy launch container inner diameter, the sonobuoy vehicle defining a sonobuoy vehicle length and a sonobuoy vehicle outer diameter; and operatively replace a substantially cylindrical external housing that is operatively adapted to substantially surround the sonobuoy internal module, the external housing defining an external housing length and an external housing outer diameter, the sonobuoy vehicle length not exceeding the external housing length, the sonobuoy vehicle outer diameter not exceeding the sonobuoy launch container inner diameter; the sonobuoy glide harness comprising; a stabilization parachute adapted to provide stabilization of the sonobuoy vehicle while the sonobuoy vehicle is in flight; a stabilization parachute ejection mechanism adapted to, while the sonobuoy vehicle is in flight, release the stabilization parachute from the sonobuoy vehicle; a plurality of deployable aerodynamic control surfaces; an actuation system operatively adapted to deploy the plurality of deployable aerodynamic control surfaces during and/or after launch of the sonobuoy vehicle from a flying aircraft; a guidance system operatively adapted to provide a dynamically determined, substantially controlled, and substantially guided descent of the sonobuoy vehicle from a release altitude, latitude, and longitude located within a predetermined release zone and toward a predetermined sonobuoy water entry zone that is defined by a predetermined range of water entry longitudes and a predetermined range of water entry latitudes; and an aerodynamic control surface ejection mechanism adapted to substantially simultaneously release the aerodynamic control surfaces from the sonobuoy vehicle and deploy a terminal parachute. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21)
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22. A method comprising:
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providing a dynamically determined, substantially controlled, and substantially guided descent of a sonobuoy vehicle from an arbitrary release altitude, latitude, and longitude located within a predetermined release zone and toward a predetermined sonobuoy water entry zone that is defined by a predetermined range of water entry longitudes and a predetermined range of water entry latitudes, the sonobuoy vehicle comprising a substantially cylindrical sonobuoy glide harness adapted to; be operably connected to a substantially cylindrical sonobuoy internal module to form the sonobuoy vehicle, the sonobuoy vehicle adapted to launch from a sonobuoy launch container that defines a sonobuoy launch container inner diameter, the sonobuoy vehicle defining a sonobuoy vehicle length and a sonobuoy vehicle outer diameter; and operatively replace a substantially cylindrical external housing that is operatively adapted to substantially surround the sonobuoy internal module, the external housing defining an external housing length and an external housing outer diameter, the sonobuoy vehicle length not exceeding the external housing length, the sonobuoy vehicle outer diameter not exceeding the sonobuoy launch container inner diameter; wherein the sonobuoy glide harness comprises; a stabilization parachute adapted to provide stabilization of the sonobuoy vehicle while the sonobuoy vehicle is in flight; a stabilization parachute ejection mechanism adapted to, while the sonobuoy vehicle is in flight, release the stabilization parachute from the sonobuoy vehicle; a plurality of deployable aerodynamic control surfaces; an actuation system operatively adapted to deploy the plurality of deployable aerodynamic control surfaces during and/or after launch of the sonobuoy vehicle from a flying aircraft; a guidance system operatively adapted to provide the dynamically determined, substantially controlled, and substantially guided descent of the sonobuoy vehicle from the arbitrary release altitude, latitude, and longitude located within the predetermined release zone and toward the predetermined sonobuoy water entry zone that is defined by the predetermined range of water entry longitudes and the predetermined range of water entry latitudes; and an aerodynamic control surface ejection mechanism adapted to substantially simultaneously release the aerodynamic control surfaces from the vehicle and deploy a terminal parachute.
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23. A machine-readable medium storing machine-implementable instructions for activities comprising:
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providing a dynamically determined, substantially controlled, and substantially guided descent of the sonobuoy vehicle from an arbitrary release altitude, latitude, and longitude located within a predetermined release zone and toward a predetermined sonobuoy water entry zone that is defined by a predetermined range of water entry longitudes and a predetermined range of water entry latitudes, the sonobuoy vehicle comprising a substantially cylindrical sonobuoy glide harness adapted to; be operably connected to a substantially cylindrical sonobuoy internal module to form the sonobuoy vehicle, the sonobuoy vehicle adapted to launch from a sonobuoy launch container that defines a sonobuoy launch container inner diameter, the sonobuoy vehicle defining a sonobuoy vehicle length and a sonobuoy vehicle outer diameter; and operatively replace a substantially cylindrical external housing that is operatively adapted to substantially surround the sonobuoy internal module, the external housing defining an external housing length and an external housing outer diameter, the sonobuoy vehicle length not exceeding the external housing length, the sonobuoy vehicle outer diameter not exceeding the sonobuoy launch container inner diameter; wherein the sonobuoy glide harness comprises; a stabilization parachute adapted to provide stabilization of the sonobuoy vehicle while the sonobuoy vehicle is in flight; a stabilization parachute ejection mechanism adapted to, while the sonobuoy vehicle is in flight, release the stabilization parachute from the sonobuoy vehicle; a plurality of deployable aerodynamic control surfaces; an actuation system operatively adapted to deploy the plurality of deployable aerodynamic control surfaces during and/or after launch of the sonobuoy vehicle from a flying aircraft; a guidance system operatively adapted to provide the dynamically determined, substantially controlled, and substantially guided descent of the sonobuoy vehicle from the arbitrary release altitude, latitude, and longitude located within the predetermined release zone and toward the predetermined sonobuoy water entry zone that is defined by the predetermined range of water entry longitudes and the predetermined range of water entry latitudes; and an aerodynamic control surface ejection mechanism adapted to substantially simultaneously release the aerodynamic control surfaces from the vehicle and deploy a terminal parachute.
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24. A circuit comprising:
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a guidance sub-circuit adapted to provide a dynamically determined, substantially controlled, and substantially guided descent of the sonobuoy vehicle from an arbitrary release altitude, latitude, and longitude located within a predetermined release zone and toward a predetermined sonobuoy water entry zone that is defined by a predetermined range of water entry longitudes and a predetermined range of water entry latitudes, the sonobuoy vehicle comprising a substantially cylindrical sonobuoy glide harness adapted to; be operably connected to a substantially cylindrical sonobuoy internal module to form the sonobuoy vehicle, the sonobuoy vehicle adapted to launch from a sonobuoy launch container that defines a sonobuoy launch container inner diameter, the sonobuoy vehicle defining a sonobuoy vehicle length and a sonobuoy vehicle outer diameter; and operatively replace a substantially cylindrical external housing that is operatively adapted to substantially surround the sonobuoy internal module, the external housing defining an external housing length and an external housing outer diameter, the sonobuoy vehicle length not exceeding the external housing length, the sonobuoy vehicle outer diameter not exceeding the sonobuoy launch container inner diameter; wherein the sonobuoy glide harness comprises; a stabilization parachute adapted to provide stabilization of the sonobuoy vehicle while the sonobuoy vehicle is in flight; a stabilization parachute ejection mechanism adapted to, while the sonobuoy vehicle is in flight, release the stabilization parachute from the sonobuoy vehicle; a plurality of deployable aerodynamic control surfaces; an actuation system operatively adapted to deploy the plurality of deployable aerodynamic control surfaces during and/or after launch of the sonobuoy vehicle from a flying aircraft; a guidance system operatively adapted to provide the dynamically determined, substantially controlled, and substantially guided descent of the sonobuoy vehicle from the arbitrary release altitude, latitude, and longitude located within the predetermined release zone and toward the predetermined sonobuoy water entry zone that is defined by the predetermined range of water entry longitudes and the predetermined range of water entry latitudes; and an aerodynamic control surface ejection mechanism adapted to substantially simultaneously release the aerodynamic control surfaces from the vehicle and deploy a terminal parachute.
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Specification