2021
DOI: 10.1007/s10846-020-01300-2
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Design and Development of a High-Speed UAS for beyond Visual Line-of-Sight Operations

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Cited by 8 publications
(3 citation statements)
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“…The helicopter system allowed us to obtain aerial imagery over much larger areas with a spatial resolution equivalent to what we can obtain with sUAS platforms and also allowed us to collect imagery in areas that were chronically cloudy and challenging to image acquisition using satellite platforms. Within the near future, with more capable platforms and changes to the regulatory framework for beyond visual line of sight operations [59,60], we anticipate replacing the manned helicopter imaging system with a UAS platform. Until that time, in Hawai'i and other places with rugged and remote terrain and persistent cloud cover, helicopter-based imaging systems can support a variety of conservation and land management needs over landscape scales [61][62][63].…”
Section: Confidence Ratings and Laboratory Sample Resultsmentioning
confidence: 99%
“…The helicopter system allowed us to obtain aerial imagery over much larger areas with a spatial resolution equivalent to what we can obtain with sUAS platforms and also allowed us to collect imagery in areas that were chronically cloudy and challenging to image acquisition using satellite platforms. Within the near future, with more capable platforms and changes to the regulatory framework for beyond visual line of sight operations [59,60], we anticipate replacing the manned helicopter imaging system with a UAS platform. Until that time, in Hawai'i and other places with rugged and remote terrain and persistent cloud cover, helicopter-based imaging systems can support a variety of conservation and land management needs over landscape scales [61][62][63].…”
Section: Confidence Ratings and Laboratory Sample Resultsmentioning
confidence: 99%
“…In this paper we focus on the lift and drag curves at low mach numbers, as they are the starting point of most performance calculations, operational simulations and contingency analyses. There is a rich literature around the estimation of drag curves on small, uncrewed, fixed wing platforms, ranging from methods based on battery energy depletion [1], to thrust estimation [2][3][4][5][6] and to methods involving unpowered manoeuvres [7][8][9][10][11]. We are, however, not aware of any systematic comparisons of these methods, in terms of their accuracy and ease of implementation, and filling this gap is the goal of this paper.…”
Section: Introductionmentioning
confidence: 99%
“…), the on-board intelligence of the autopilot must be able to re-plan its tasking accordingly (ideally with error margins attached, obtained, for example, through an ensemble of Monte Carlo runs of the performance model). Once again, attempting to do this with with rudimentary baseline performance guesses carries vast penalties in terms of unnecessarily conservative fuel reserves (such as McCrink and Gregory [7] who took off with ∼ 190% more fuel than the mass calculated to complete the mission), unnecessarily aborted missions, or, worse, accidents caused by fuel starvation.…”
Section: Introductionmentioning
confidence: 99%