Browse Topic: Global positioning systems (GPS)
Emerging microelectronic technologies are expanding functionalities for future decades of vertical lift platforms, enabling both manned and unmanned rotorcraft to fully and safely participate in the NextGen National Airspace System. Specifically, for rotorcraft, benefits from expanded multi-functionality and reduced weight and space requirements, for both mandatory and desired optional avionics, are entering advanced development and flight-testing stages prior to being available to all users. One has only to think about the incredible, multifunctional capabilities of a smartphone to imagine what is possible in avionics with today's advanced technology. This presentation discusses achievements that only a few years ago were beyond imagination – miniaturized avionics that fully employ tiny but powerful digital processors and software defined multi-functional systems on a single chip are rapidly obsoleting the "black boxes" of the past. For both manned and unmanned rotorcraft systems, the benefits must be validated; and when proven valid, are immense in terms of lighter weight, tiny form factors, and lower costs. This presentation also addresses validation of ADS-B2, which depends on verification of GPS signals with technological approaches that counter potential malicious spoofing, jamming and interference.
ABSTRACT This paper describes the use of a low-cost standalone MEMS-IMU (micro-electromechanical system - inertial measurement unit) sensor system developed by the National Research Council Canada (NRC) for manoeuvre recognition in helicopters. The system records accelerations, angular rotation rates, magnetic flux, altitude, location and velocity through its IMU and GPS. The MEMS-IMU system was flown on the Bell 412 CH-146 Griffon helicopter in a series of scripted flights consisting of 60 manoeuvres and regimes from the helicopter's usage spectrum. A flight log recorded by passengers with detailed start and stop times and identification of the manoeuvres during flight was key information in the development of manoeuvre recognition models. Statistical tests to analyze the data diversity between each flight showed significant variability of the parameters from flight to flight. Because of this variability and because there was significant imbalance in the distribution of data for the individual manoeuvres, a pooled stratified sampling scheme was used to construct a representative training set for developing data-driven models. Different subsets of the MEMSIMU measurements were explored to exclude GPS and/or magnetometer readings. Even with the different subsets, the classifier results using stratified sampling show that very high overall classification accuracy can be obtained using the measurements from the standalone MEMS-IMU sensor system.
This document recommends criteria for the design and installation of Autopilot, Flight Director and Autothrust Systems. These three systems are highly interrelated and will be referred to generically as an Integrated Flight Guidance System (IFGS).
Rotorcraft operating in unprepared locations must be capable of safe flight in the presence of unmapped obstacles and absence of GPS, and must be able to quickly and reliably assess a potential landing zone's suitability for landing. This paper presents technologies that address these needs and the result of their application to an actual unmanned helicopter prototype.
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