Optimization of vertical plane cobralike pitch reversal maneuvers

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 4, 2002, Pages 693-702

  Komduur, H J ^a,b   Visser, H G ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b TNO   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; CLOSED LOOP CONTROL SYSTEMS; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; NONLINEAR CONTROL SYSTEMS; NONLINEAR PROGRAMMING; RESEARCH AIRCRAFT;

THRUST VECTORING;

MANEUVERABILITY;

EID: 0036640860     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4936     Document Type: Article

References (13)

1. X.31 kill ratios exceed predictions
2. Agile sukhoi Su-27 leads strong soviet presentation
3. Mathematical phenomenology for thrust-vectoring-induced agility comparisons
4. The cobra maneuver as a minimum time problem
5. Optimization for fighter aircraft vertical-plane maneuvering using poststall flight
6. Minimum-time maneuvers of thrust-vectored aircraft
7. An elementary proof of a functional analysis result having interest for minimax optimal control of aeroassisted orbital transfer vehicles
8. Thrust vectoring on the NASA F-18 high alpha research vehicle
9. Classical turning performance of a fighter aircraft revisited
10. Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives
11. The F-18 high alpha research vehicle: A high-angle-of-attack testbed aircraft
12. Nonlinear inversion flight control for supermaneuverable aircraft
13. Discrete approximations to optimal trajectories using direct transcription and nonlinear programming