Abstract: A flying vehicle comprises an elongated airfoil having a first end and a second end defining a longitudinal axis, the first and second ends further defining an interior opening extending therebetween and terminating at an outlet port proximal the second end; a solid fuel engine includes a fuel combustion chamber proximal the first end of the airfoil; a first manifold is coupled to the fuel combustion chamber and configured to convey a pressurized gas generated by combustion of a solid fuel; wherein the interior opening conveys the pressurized gas from the first manifold to the outlet port proximal the second end and wherein the pressurized gas is exhausted at the outlet port substantially perpendicular to the longitudinal axis of the elongated airfoil, thereby producing thrust which imparts a rotational motion to the airfoil about a center of mass proximal to the first end, for thereby defining a rotor disk.

Abstract: An unmanned aerial vehicle (UAV) has a payload or body affixed at one end of an elongated airfoil. The entire airfoil/payload combination rotates about a center of mass to define a rotor disk. Thrust is provided by air-augmented rocket engine thrusting tangentially at a location remote from the payload. A control system maintains knowledge of its environment, as by a camera, to produce directional control signals which actuate lift control means in synchronism with the rotational position of the vehicle. A deployable object may be carried. Protection of the stowed vehicle is provided by blister packaging.

Abstract: A system controls a team of vehicles. The system includes a plan dependency identifier, a contingency monitor, and an alert formulator. The plan dependency identifier analyzes a mission plan and identifies mission constraints of the mission plan. The contingency monitor continuously reviews execution of the mission plan for violations of the mission constraints. The alert formulator determines whether a part of the mission plan is threatened by a violation of one of the mission constraints.

Abstract: A system controls a team of vehicles. The system includes a plan dependency identifier, a contingency monitor, and an alert formulator. The plan dependency identifier analyzes a mission plan and identifies mission constraints of the mission plan. The contingency monitor continuously reviews execution of the mission plan for violations of the mission constraints. The alert formulator determines whether a part of the mission plan is threatened by a violation of one of the mission constraints.

Abstract: An unmanned aerial vehicle (UAV) has a payload or body affixed at one end of an elongated airfoil. The entire airfoil/payload combination rotates about a center of mass to define a rotor disk. Thrust is provided by air-augmented rocket engine thrusting tangentially at a location remote from the payload. A control system maintains knowledge of its environment, as by a camera, to produce directional control signals which actuate lift control means in synchronism with the rotational position of the vehicle. A deployable object may be carried. Protection of the stowed vehicle is provided by blister packaging.

Abstract: A system collaboratively and autonomously plans and controls a team of unmanned vehicles within an environment. A mission planning component creates a mission plan for a plurality of members of the team of unmanned vehicles. The mission planning component creates a task plan for each member based on the mission plan. A collaboration component assigns members to the team and roles for the assigned members. The collaboration component updates membership and roles of the members based on the changing situation of the environment. A situational awareness component evaluates the changing situation of the environment based on information from the assigned members of the team. A contingency management component monitors the changing situation of the environment. The contingency management component monitors changes of capabilities of the assigned members of the team and execution of the mission plan and task plans.