TY - GEN
T1 - Piloted Evaluation of Adaptive Flight Controls Designed to Improve Performance, Safety, and Survivability for Advanced VTOL Aircraft
AU - Bridges, Derek O.
AU - Berger, Tom
AU - Horn, Joseph F.
AU - Hagwood, D. Grey
N1 - Publisher Copyright:
Copyright © 2021 by the Vertical Flight Society. All rights reserved.
PY - 2021
Y1 - 2021
N2 - ADAPT™ is a flight control software package that improves the safety, survivability, performance, and affordability of advanced VTOL aircraft that include multiple types and instances of control effectors. ADAPT™ includes three different control algorithms: Fly-to-Optimal performs trim optimization based on selected objectives for increased performance; Vehicle Maneuver Optimization improves maneuverability in unsteady flight; Damage Tolerant Control re-allocates control forces and moments to allow for a greater chance of survival in case of damage to the aircraft. This paper describes the implementation and testing of these algorithms in piloted simulation of an operational mission using the X-49 winged compound aircraft. The results show that, with ADAPT™ on, the operational mission can be flown faster while burning less fuel, resulting in increased aircraft endurance and range. Maneuvering flight with ADAPT™ can be flown faster as well. In the case of simulated aircraft damage, aircraft without ADAPT™ were unable to recover and crashed in every case tested, while those with ADAPT™ were able to recover, fly to an emergency airfield, and land.
AB - ADAPT™ is a flight control software package that improves the safety, survivability, performance, and affordability of advanced VTOL aircraft that include multiple types and instances of control effectors. ADAPT™ includes three different control algorithms: Fly-to-Optimal performs trim optimization based on selected objectives for increased performance; Vehicle Maneuver Optimization improves maneuverability in unsteady flight; Damage Tolerant Control re-allocates control forces and moments to allow for a greater chance of survival in case of damage to the aircraft. This paper describes the implementation and testing of these algorithms in piloted simulation of an operational mission using the X-49 winged compound aircraft. The results show that, with ADAPT™ on, the operational mission can be flown faster while burning less fuel, resulting in increased aircraft endurance and range. Maneuvering flight with ADAPT™ can be flown faster as well. In the case of simulated aircraft damage, aircraft without ADAPT™ were unable to recover and crashed in every case tested, while those with ADAPT™ were able to recover, fly to an emergency airfield, and land.
UR - https://www.scopus.com/pages/publications/85167715015
UR - https://www.scopus.com/pages/publications/85167715015#tab=citedBy
M3 - Conference contribution
AN - SCOPUS:85167715015
T3 - Modern Operations with Future Integrated Vehicle Management Systems 2021
SP - 1
EP - 17
BT - Modern Operations with Future Integrated Vehicle Management Systems 2021
PB - Vertical Flight Society
T2 - 2021 Modern Operations with Future Integrated Vehicle Management Systems
Y2 - 19 August 2021 through 20 August 2021
ER -