Abstract: A system in accordance with the present invention tasks a team of autonomous unmanned vehicles. The system includes a first team member and a second team member. The first team member has a first level of autonomy. The second team member has a second level of autonomy. The first level of autonomy is different than the first level of autonomy. The first team member is given instructions corresponding to the first level of autonomy. The second team member is given instructions corresponding to the second level of autonomy.

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.

Abstract: A system in accordance with the present invention tasks a team of autonomous unmanned vehicles. The system includes a first team member and a second team member. The first team member has a first level of autonomy. The second team member has a second level of autonomy. The first level of autonomy is different than the first level of autonomy. The first team member is given instructions corresponding to the first level of autonomy. The second team member is given instructions corresponding to the second level of autonomy.

Abstract: A flyer assembly is adapted for launching with, transit in, and deployment from an artillery shell having a central void region extending along a ballistic shell axis. The flyer assembly includes a jettisonable shroud and a flyer. The shroud extends along a shroud axis, and is positionable within the central void region with the shroud axis substantially parallel to the shell axis. The flyer is adapted to withstand a launch acceleration force along a flyer axis when in a first state, and to effect aerodynamic flight when in a second state. When in the first state, the flyer is positionable within the shroud with the flyer axis parallel to the shroud axis and the shell axis. The flyer includes a body member disposed about the flyer axis, and a foldable wing assembly mounted to the body member. The wing assembly is configurable in a folded state characterized by a plurality of nested wing segments when the flyer is in the first state.

Abstract: A flyer assembly is adapted for launching with, transit in, and deployment from an artillery shell having a central void region extending along a ballistic shell axis. The flyer assembly includes a jettisonable shroud and a flyer. The shroud extends along a shroud axis, and is positionable within the central void region with the shroud axis substantially parallel to the shell axis. The flyer is adapted to withstand a launch acceleration force along a flyer axis when in a first state, and to effect aerodynamic flight when in a second state. When in the first state, the flyer is positionable within the shroud with the flyer axis parallel to the shroud axis and the shell axis. The flyer includes a body member disposed about the flyer axis, and a foldable wing assembly mounted to the body member. The wing assembly is configurable in a folded state characterized by a plurality of nested wing segments when the flyer is in the first state.

Abstract: A flyer assembly is adapted for launching with, transit in, and deployment from an artillery shell having a central void region extending along a ballistic shell axis. The flyer assembly includes a jettisonable shroud and a flyer. The shroud extends along a shroud axis, and is positionable within the central void region with the shroud axis substantially parallel to the shell axis. The flyer is adapted to withstand a launch acceleration force along a flyer axis when in a first state, and to effect aerodynamic flight when in a second state. When in the first state, the flyer is positionable within the shroud with the flyer axis parallel to the shroud axis and the shell axis. The flyer includes a body member disposed about the flyer axis, and a foldable wing assembly mounted to the body member. The wing assembly is configurable in a folded state characterized by a plurality of nested wing segments when the flyer is in the first state.