With a focus on updating the Peregrine I UAV for remote mapping applications, the primary goal for this academic year is to optimize the fixed-wing configuration to achieve flight. The team is working towards finalizing, building, and flight-testing the updated design of the aircraft. The following steps outline the work involved this year:<\/p>\n
Several key design changes were made to improve the performance and capabilities of the Peregrine I for remote flight and mapping. This includes integrating flexible solar panels into the wings to extend flight endurance, optimizing the aircraft\u2019s structural components for weight reduction and strength, and transitioning the airframe to support conventional fixed-wing flight. Additionally, the landing gear was redesigned to enhance durability and ground handling for the new configuration.<\/p>\n
The CAD model of the Peregrine I was transferred from SolidWorks to CATIA to leverage industry-standard 3D CAD tools. This transition allowed for the refinement of the outer mold line (OML) and structural analysis by the Stress Engineering team. The Loads and Dynamics teams provided critical input on load cases and flight stability, enabling the finalization of the design. Stress distribution maps were created with Altair Hypermesh to guide material removal in low-stress areas, further reducing weight while maintaining structural integrity.<\/p>\n
Once the design was finalized, the Additive Manufacturing team began 3D printing key components using PET-G filament. The Systems and Avionics teams coordinated the installation and testing of electronic components, including power management systems linked to the solar panels. Meanwhile, the Assembly team prepared to fit and assemble all components into the final UAV structure.<\/p>\n
After the aircraft’s assembly is complete, it will undergo flight testing. The Avionics, Performance, and Control Laws teams will collaborate to define the flight control system and establish the test parameters. The aircraft’s autonomous flight capabilities and conventional fixed-wing performance will be tested, with data collected to validate the design and identify improvements for future iterations, including the development of the larger Peregrine II.<\/p>\n","protected":false},"excerpt":{"rendered":"
With a focus on updating the Peregrine I UAV for remote mapping applications, the primary goal for this academic year is to optimize the fixed-wing configuration to achieve flight. The team is working towards finalizing, building, and flight-testing the updated design of the aircraft. The following steps outline the work involved this year: Design Changes […]<\/p>\n","protected":false},"author":5,"featured_media":0,"parent":0,"menu_order":2,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_relevanssi_hide_post":"","_relevanssi_hide_content":"","_relevanssi_pin_for_all":"","_relevanssi_pin_keywords":"","_relevanssi_unpin_keywords":"","_relevanssi_related_keywords":"","_relevanssi_related_include_ids":"","_relevanssi_related_exclude_ids":"","_relevanssi_related_no_append":"","_relevanssi_related_not_related":"","_relevanssi_related_posts":"","_relevanssi_noindex_reason":"","_mi_skip_tracking":false,"_exactmetrics_sitenote_active":false,"_exactmetrics_sitenote_note":"","_exactmetrics_sitenote_category":0,"_monsterinsights_sitenote_active":false,"_monsterinsights_sitenote_note":"","_monsterinsights_sitenote_category":0,"footnotes":"","_links_to":"","_links_to_target":""},"yoast_head":"\n