Flight control laws for NASA's hyper-X research vehicle

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 1-11

  Davidson, J ^a   Lallman, F ^a   McMinn, J D ^a   Martin, J ^a   Pahle, J ^b   Stephenson, M ^b   Selmon, J ^c   Bose, D ^d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^c BOEING COMPANY   (United States)

^d Analytical Methods and Associates   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; CONTRACTS; CONTROL SYSTEM SYNTHESIS; FLIGHT CONTROL SYSTEMS; HYDROGEN FUELS; HYPERSONIC VEHICLES; NASA; PROPULSION; RAMJET ENGINES; VEHICLE PERFORMANCE;

DESCENT TRAJECTORIES; ENABLING TECHNOLOGIES; FLIGHT CONTROL LAW; FLIGHT DEMONSTRATION; PERFORMANCE PREDICTION; ROBUSTNESS ANALYSIS; STABILITY MARGINS; SUPERSONIC COMBUSTION;

SUPERSONIC AIRCRAFT;

EID: 84959099708     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4124     Document Type: Conference Paper

References (6)

1. Lallman, F.; Davidson, J.; and Pahle, J.: Hyper-X Government Furnished Items (NASl-97110): Preliminary (inner loop) Control Laws for Candidate Design, Deliverable H7006-M7-01-GCT, March 24, 1997, NASA Report HXGFI-001.
2. McClinton, et al.: NASA's Hyper-X Program. Presented at the 1997 JANNAF Joint Meetings, West Palm Beach, Florida, October 27-31, 1997.
3. Morelli, E. A.: Flight Test Validation of Optimal Input Design and Comparison to Conventional Inputs. AIAA 973711, AIAA AFM Conference, August 11-13, 1997. New Orleans, LA.
4. Ogata, K.: Modern Control Engineering. Prentice-Hall, Inc., 1970.
5. Selmon, J.; Bose, D.; and Miranda, L.: Hyper-X Critical design Review: Flight Controls. Presented at Hyper-X Critical Design Review, Seal Beach, CA. February 2-5, 1998.
6. White, IT.: Recommended HX-FADS Configuration/NASA Report HX-387, NASA Dryden Flight Research Center, September 1997.