Bio-Inspired Rotating Empennage
Funded by the Air Force Research Lab
January 2020 - December 2025
Table of Contents
Project Overview
Birds control lateral maneuvers without a vertical tail. The goal of the present work is to evaluate whether aircraft can be controlled with a bio-inspired rotating empennage (rotating horizontal tail).
In theory, the forces and moments produced by the empennage can be summed to a single force vector and moment vector. By rotating a horizontal stabilizer and deflecting the elevator, the same force and moment vectors should be able to be created without a vertical tail.
Flight Simulation
We have developed a flight simulator to evaluate the static and dynamic stability and controls of the BIRE variant of the F-16 compared to the baseline aircraft.
V1.1: Full F-16 Simulator
January 2023
Features:
Updated aerodynamic model, including Prandtl-Glauert compressibility corrections
Direct surface / throttle control using keyboard, gamepad, or joystick input
Full HUD including flight path vector, radar altitude, mach number, and control surface indicators
Spring-damper landing physics using terrain ray casts
3rd person, cockpit, and toggleable alternate camera views
Flight Testing
Volantex Flight Test #2
October 7, 2021
Purpose: Test retractable vertical stabilizer and rotating horizontal stabilizer.
Glider Flight Test #1
July 23, 2024
Purpose:
Test hardware, software, and ground station on simple aircraft
Verify pilot command response time
Verify ground station link and live plotting
Verify data logging on SD card and ground station
Outcome: Successful flight. All comms working correctly. Tested both manual mode and flight controller mode. Ground station link and live plotting worked correctly. Data logging onboard and on ground worked correctly. Landed a little too slow. Aircraft stalled just before touchdown. No damage to airframe or sensors. Some control surfaces are sticking due to construction. Will construct new glider for next flight.
Flight Time: 00:06:11
Glider Flight Test #2
August 6, 2024
Purpose:
Test newly built glider
Test IMU sensor
Test Pitot sensor
Test onboard and ground logging of sensors
Ground station plotting of sensor data (heading, pqr, airspeed)
Outcome:
Flight Time:
Publications
Journal Publications
A Review of Avian-Inspired Morphing for UAV Flight Control
Harvey, C., Gamble, L. L., Bolander C. R., Hunsaker, D. F., Joo, J. J., and Inman, D. J., "A review of avian-inspired morphing for UAV flight control," Progress in Aerospace Sciences, 2022, 27 pages, DOI: 10.1016/j.paerosci.2022.100825
Conference Publications
Evaluation of First-Order Actuator Dynamics and Linear Controller for a Bio-Inspired Rotating Empennage Fighter Aircraft
Moulton, B. C., Harris, M. W., Hunsaker, D. F., and Joo, J. J., “Evaluation of First-Order Actuator Dynamics and Linear Controller for a Bio-Inspired Rotating Empennage Fighter Aircraft,” AIAA SciTech 2024 Forum, January 2024, AIAA-2024-2649 DOI: 10.2514/6.2024-2649
Attainable Moment Set and Actuation Time of a Bio-Inspired Rotating Empennage
Bolander, Christian R., et al. "Attainable Moment Set and Actuation Time of a Bio-Inspired Rotating Empennage." AIAA SCITECH 2022 Forum. 2022. DOI: 10.2514/6.2022-1670
Static Trim of a Bio-Inspired Rotating Empennage for a Fighter Aircraft
Bolander, C. R., Kohler, A. J., Hunsaker, D. F., Myszka, D., and Joo, J. J., “Static Trim of a Bio-Inspired Rotating Empennage for a Fighter Aircraft,” AIAA SCITECH 2023 Forum, 2023, p. 0624. DOI: 10.2514/6.2023-0624
Linearized Rigid-Body Static and Dynamic Stability Of An Aircraft With A Bio-Inspired Rotating Empennage
Kohler, A. J., Bolander, C. R., Hunsaker, D. F., and Joo, J. J., “Linearized Rigid-Body Static and Dynamic Stability Of An Aircraft With A Bio-Inspired Rotating Empennage,” AIAA SciTech 2022 forum, 2022, DOI: 10.2514/6.2023-0621
Theses and Dissertations
Aerodynamic Implications of a Bio-Inspired Rotating Empennage Design for Control of a Fighter Aircraft
Bolander, Christian R., "Aerodynamic Implications of a Bio-Inspired Rotating Empennage Design for Control of a Fighter Aircraft" (2022). All Graduate Theses and Dissertations. 8749.
Linearized Rigid-Body Static and Dynamic Stability of an Aircraft With a Bio-Inspired Rotating Empennage
Kohler, Austin J., "Linearized Rigid-Body Static and Dynamic Stability of an Aircraft With a Bio-Inspired Rotating Empennage" (2022). All Graduate Theses and Dissertations. 8675.
Students
PhD
Christian Bolander
Ben Moulton
MS
Austin Kohler
Ashton Gilbert
Kathle Tischner
Undergraduate
Spencer Adams