Advanced Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles
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Home > Reference > Research and information: general > Research methods: general > Advanced Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles
Advanced Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles

Advanced Aeroservoelastic Stabilization Techniques for Hypersonic Flight Vehicles


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About the Book

Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicles, that are statically unstable, require higher bandwidth flight control systems to compensate for the instability resulting in interactions between the flight control system, the engine/propulsion dynamics, and the low frequency structural modes. Military specifications, such as MIL-F-9490D and MIL-F-87242, tend to limit treatment of structural modes to conventional gain stabilization techniques. The conventional gain stabilization techniques, however, introduce low frequency effective time delays which can be troublesome from a flying qualities standpoint. These time delays can be alleviated by appropriate blending of gain and phase stabilization techniques (referred to as Hybrid Phase Stabilization or HPS) for the low frequency structural modes. The potential of using HPS for compensating structural mode interaction was previously explored. It was shown that effective time delay was significantly reduced with the use of HPS; however, the HPS design was seen to have greater residual response than a conventional gain stablized design. Additional work performed to advance and refine the HPS design procedure, to further develop residual response metrics as a basis for alternative structural stability specifications, and to develop strategies for validating HPS design and specification concepts in manned simulation is presented. Stabilization design sensitivity to structural uncertainties and aircraft-centered requirements are also assessed. Chan, Samuel Y. and Cheng, Peter Y. and Myers, Thomas T. and Klyde, David H. and Magdaleno, Raymond E. and Mcruer, Duane T. Unspecified Center AEROSERVOELASTICITY; AIRCRAFT CONTROL; DESIGN ANALYSIS; DYNAMIC MODELS; DYNAMIC STRUCTURAL ANALYSIS; FLEXIBLE SPACECRAFT; FLIGHT CONTROL; HYPERSONIC VEHICLES; STABILIZATION; STRUCTURAL STABILITY; FLIGHT CHARACTERISTICS; FREQUENCY RESPONSE; HUMAN FACTORS ENGINEERING; SINGLE STAGE TO ORBIT VEHI...


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Product Details
  • ISBN-13: 9781722919559
  • Publisher: Createspace Independent Publishing Platform
  • Publisher Imprint: Createspace Independent Publishing Platform
  • Height: 279 mm
  • No of Pages: 120
  • Spine Width: 6 mm
  • Width: 216 mm
  • ISBN-10: 1722919558
  • Publisher Date: 17 Jul 2018
  • Binding: Paperback
  • Language: English
  • Returnable: N
  • Weight: 295 gr


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