Abstract: Apparatuses, systems, and methods are provided for transplanting slips with an automated slip transplanter. The transplanter comprises a planter unit, a singulation unit, a conveyor belt, a node sensor, and a controller. The planter unit is configured to plant consistent rows of evenly spaced slips in a field. The singulation unit comprises automated grippers and slip cartridges, and is configured to continuously singulate harvested slips stored in the slip cartridges. The conveyor belt is configured to receive the singulated slips from the automated grippers with brushed holders, and transfer the received slips on a belt to the planter unit. The node sensor is configured to autonomously collect performance data of the singulated slips in real-time. The controller is communicatively coupled to the node sensor, and configured to implement operational modes and dynamically adjust a planting slip rate based on the operational modes and performance data collected by the node sensor.

Abstract: An apparatus and methods are provided for transplanting slips with an automated slip transplanter. The transplanter comprises a planter unit, a singulation unit, a conveyor belt, a node sensor, and a controller. The planter unit is configured to plant consistent rows of evenly spaced slips in a field. The singulation unit comprises automated grippers and slip cartridges, and is configured to continuously singulate harvested slips stored in the slip cartridges. The conveyor belt is configured to receive the singulated slips from the automated grippers with brushed holders, and transfer the received slips on a belt to the planter unit. The node sensor is configured to autonomously collect performance data of the singulated slips in real-time. The controller is communicatively coupled to the node sensor, and configured to implement operational modes and dynamically adjust a planting slip rate based on the operational modes and performance data collected by the node sensor.

Abstract: Embodiments of systems, devices, and methods are described that relate to module structures for use in forming a cabin interior of an aircraft. Many embodiments relate to a support structure including a lattice configurable to provide a standardizable frame for connection to the interior of the aircraft and to provide a space within the frame in which module fixtures can be positioned and secured to the frame. Embodiments of the support structure can include a floor with a number of structures and devices that can be used to provide support for the module and secure the module to the floor of the aircraft fuselage. Embodiments of transport systems for the modules are also described and such can be integrated with the floor of the module such that the modules transport mechanism, or a significant portion thereof, is contained within the module itself.