Optimization of aircraft spin recovery maneuvers
Authors:
- D.M.K.K. Venkateswara RaoDRD.M.K.K. Venkateswara Rao
- Tiauw H. GoTGTiauw H. Go
- 1 July 2019
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 90, 222-232
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- On the development of flight-test equipment in relation to the aircraft spinProgress in Aerospace Sciences, 2018
- Reinforcement Learning-Based Optimal Flat Spin Recovery for Unmanned Aerial VehicleJournal of Guidance, Control, and Dynamics, 2017
- A sliding mode controller for aircraft simulated entry into spinAerospace Science and Technology, 2013
- Autorotational Spin Evolving Towards ChaosJournal of Aircraft, 2012
- Aircraft Spin Recovery Using a Sliding-Mode ControllerJournal of Guidance, Control, and Dynamics, 2010
- Aircraft Spin Recovery, with and without Thrust Vectoring, Using Nonlinear Dynamic InversionJournal of Aircraft, 2005
- Momentum Vector Control for Spin RecoveryJournal of Aircraft, 2004
- Alleviation of Spin-Entry Tendencies through Localization of Wing-Flow SeparationJournal of Aircraft, 1981
- Aerodynamic Characteristics of Fighter Configurations During Spin Entries and Developed SpinsJournal of Aircraft, 1978
- Influence of the Static and Dynamic Aerodynamic Characteristics on the Spinning Motion of AircraftJournal of Aircraft, 1971