October 20, 2010 article Open access Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction Journal of Guidance Control and Dynamics DOI: 10.2514/1.49978 Full text (OA) OpenAlex Authors 0 Author list not loaded yet. Cited by 2 stored of 491 Search Sort Most cited Newest Oldest Patent citations Title Any typearticle review book-chapter conference-paper preprint dissertation book dataset other Any fieldAgricultural and Biological Sciences Arts and Humanities Biochemistry, Genetics and Molecular Biology Business, Management and Accounting Chemical Engineering Chemistry Computer Science Decision Sciences Dentistry Earth and Planetary Sciences Economics, Econometrics and Finance Energy Engineering Environmental Science Health Professions Immunology and Microbiology Materials Science Mathematics Medicine Neuroscience Nursing Pharmacology, Toxicology and Pharmaceutics Physics and Astronomy Psychology Social Sciences Veterinary Open access Flight Control Architecture of a Flying Wing for Vertical Take-Off and Landing of an Airborne Wind Energy System 2021 AIAA SciTech Forum conference-paper Engineering Aerospace Engineering and Energy Systems 5 citations Actuator modelling for attitude control using incremental nonlinear dynamic inversion 2020 International Journal of Micro Air Vehicles article Engineering Aerospace Engineering and Control Systems Open access 8 citations 2 results References 0