US 6,119,976 AGranted

Shoulder launched unmanned reconnaissance system

OwnerMichael E. Rogersinventor

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Abstract

A shoulder launched unmanned reconnaissance system for providing overhead visual surveillance of remote targets is disclosed. The present system includes a reconnaissance air vehicle which may be fired from a portable launcher, accelerated to flight speed, and remotely controlled using a ground control system. The vehicle is flown to the target area to enable an onboard wide angle video system to transmit video images of the target by radio or fiber optics link to the ground control system for processing and display. The ground control system enables the reconnaissance vehicle to be flown to a recovery area and to descend in a stall mode after the flight is completed for maintenance prior to reuse. The air vehicle includes collapsible wings which are deployable after launch by a spring actuated mechanism. The fuselage of the air vehicle carries an onboard video camera, an electric motor, a battery, a global positioning system receiver, flight controls, and a data link system. In an alternative embodiment, the fuselage of the air vehicle includes a storage bay with a rotary mechanism capable of deploying sensors for chemical and biological warfare agents or other dropable payloads such as dye markers for marking fleeing motor vehicles. The present system is capable of conducting overhead surveillance up to a range of approximately 10 kilometers.

An unmanned reconnaissance system for surveying a remote location, comprising:

a portable elongated launch cylinder having an internal cylindrical cavity therein;
a launch vehicle telescopically slidably disposable in said cavity;
means coacting between said launch cylinder and said launch vehicle for ejecting said launch vehicle from said cavity of said launch cylinder, said launch vehicle including an elongated fuselage having a front end and a rear end, collapsible propeller means operatively carried at said front end of said fuselage, power means for operating said propeller means to propel said launch vehicle after said launch vehicle is ejected from said launch cylinder, a pair of collapsible wings carried on said fuselage between said front end and said rear end, each of said wings comprising a rear spar rotatably connected at an inner end to an outboard portion of said rear end of said fuselage at a first pivotal connection, a front spar rotatably connected at an inner end to said fuselage at a longitudinally slidable second pivotal connection located transversely between said first pivotal connections, said second pivotal connection having a pre-launch position adjacent said first pivotal connection and a post-launch position toward said front end of said fuselage, first biasing means for longitudinally shifting said second pivotal connection, from said pre-launch position to said post-launch position, second biasing means for rotating said rear spar outwardly of said fuselage, a third pivotal connection rotatably connecting outer ends of said front spar and said rear spar whereby in said pre-launch condition said rear spar and said front spar are in overlapping relationship along said fuselage, a foldable lightweight material interconnecting said front spar and said rear spar and establishing an airfoil surface in said post-launch condition, fin means pivotally carried on a lower surface of said fuselage and biased downwardly from said fuselage in said post-launch condition, camera means carried on said fuselage for providing video signals regarding said remote location, and operator controlled transceiver means for controlling said propeller means for establishing a flight path for said vehicle toward said remote location and for receiving said video signals from said camera means.

Abstract

Claims13