Intelligent Payload Module Concept Evolution

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Presentation transcript:

Intelligent Payload Module Concept Evolution Dan Mandl HyspIRI Symposium Intelligent Payload Module Session June 5, 2014

Direct Broadcast Module Original HyspIRI Low Latency Data Flow Operations Concept (Intelligent Payload Module) TIR Command & Data Handling Solid State Recorder 130.2 Mbps VSWIR 804 Mbps Intelligent Payload Module (IPM) Direct Broadcast Module Spacecraft 20 Mbps S-band command S-band Housekeeping data X-band 800 Mbps Science data Direct Broadcast Antennas To/From Alaska and Norway Ground Stations 2

Revised Low Latency Ops Concept High speed instrument data source IPM Flight Testbed SCIENCE USER SpaceCube FPGA Co-Processor Select algorithm to run Create algorithm Cloud Run Level 2 Data Product Algorithm WCPS Runtime Service WCPS Algorithm Builder Service Onboard Algorithm Buffer HyspIRI Mission concept evolving so making low latency concept more generic with some combination of ground cloud computing and onboard multicore processor. 3

Broad Range of Supported Platforms Contract MD 500C ISS Optical Window USFS King Air B200 USFS Cessna Citation HyspIRI Intelligent Payload Module Landsat 9 Rotorcraft Drone NASA Cessna 206H 4

Typical Science Algorithms Low latency users access data products via onboard Web Coverage Processing Service (WCPS) which allows specifying algorithms in real time and rapid access of resultant products Spectral Angle Mapper image classification; Regression Tree image classification; Vegetation dynamics; Water quality; Burned area; Flooded area; Habitat fragmentation; and Stretch goals like plume detection.

Exercising the Technology Use sub-orbital platforms to demonstrate the IPM architecture in real world situations; Employ computationally demanding algorithms in real time; Evaluate new processors and compilers; Pass data products to users via com links of reduced bandwidth; Coordinate collects among multiple assets; Engage with next generation design efforts for missions such as an ISS spectrometer, HyspIRI and Landsat 9 mission formulation.

Key Methods to Accelerate Onboard Computing for a Space Environment Intelligent onboard data reduction Parallel processing, multicore processors Use of FPGA as co-processor to accelerate portion of algorithms 7

Compact IPM Box for UAS Operations Modified version of IPM to install on an mini-UAV helicopter integrated by Enric Pastor of Univ. of Catalunya (co-investigator) 8 Demonstration: University of Catalunya UAV Mini-helicopter

UAS Jellyfish Monitoring Mission Autonomous Helicopter with Onboard IPM Computation 9 Demonstration: University of Catalunya UAV Mini-helicopter

Larger UAS Helicopter Being Set Up 10 Demonstration: University of Catalunya UAV Mini-helicopter

Simulation Scenario with Sierra UAS https://www.youtube.com/watch?v=aFXdxjX1DDo&feature=youtu.be Demonstration: University of Catalunya UAV Mini-helicopter 11

Unmanned Aerial System Jellyfish Monitoring Mission with IPM (Univ Unmanned Aerial System Jellyfish Monitoring Mission with IPM (Univ. of Catalunya) Area of interest: Delta del Ebre south of Barcelona. Multiple Australian jellyfish being increasingly detected. First test mission: Late summer 2012 Initial low-altitude mid-altitude images successfully acquired. Demonstration mission with IPM (containing Tilera processor) summer 2014 http://www.youtube.com/watch?v=Uam7-thvM80 12